X, The Moonshot Factory
AI-assisted summary of Pulling Power from the Sky: The Story of Makani [Feature Film] — original source. Check the original for full context.
Source published:
Key ideas
- Makani spent 13 years developing utility-scale airborne wind turbines, aiming to cut structural material by roughly 90% and cost from 20 cents to 3–4 cents per kilowatt-hour by replacing steel towers with tethered crosswind airfoils. (2:16)
- After scaling from the 20 kW Wing 7 prototype to the 600 kW M600 within Google X, the program demonstrated full autonomous flight cycles including vertical hover, crosswind generation, and robotic perch recovery. (70:25)
- Faced with plummeting land-based wind turbine costs, Makani pivoted offshore to deploy the M600 from a floating spar buoy in Norway, achieving crosswind generation over the North Sea before a trans-out crash in rough swells. (74:58)
- Despite proving crosswind flight physics and offshore feasibility, Makani shut down after spinning out from Alphabet when it could not secure commercial capital to fund multi-thousand-hour reliability testing. (98:41)
Detailed notes
## Background Published on YouTube by X, The Moonshot Factory on September 10, 2020, this feature film documents the thirteen-year journey of Makani, an eclectic team of scientists, artists, pilots, and engineers. According to the page description, the film provides an intimate portrait of the team's quest to design and build autonomous kites capable of efficiently harvesting wind power, featuring testing footage across California, Hawai’i, and Norway.
## TL;DR Founded in 2006 to drastically lower renewable energy costs, Makani sought to eliminate heavy turbine towers by harnessing high-altitude wind with tethered wings operating in continuous crosswind loops. The project evolved from simple soft foils and lightweight prototypes into the 20-kilowatt Wing 7, before scaling under Alphabet's X into the utility-class 600-kilowatt M600 system tested at China Lake and Parker Ranch. Facing changing onshore wind market economics, the team adapted their technology for deepwater offshore deployment on a floating spar buoy in the North Sea off Norway. While the team achieved historic autonomous flight milestones, persistent operational risks, an offshore crash, and immense commercial capital hurdles led to the project's closure after thirteen years.
## Atmosphere & style The film strikes a deeply earnest, bittersweet, and technologically reverent tone, capturing both the chaotic grit of prototype fabrication and the quiet poetry of flight. Viewers are immersed in the emotional volatility of hardware development—from the anxious exhaustion of grounded test windows and the shock of catastrophic airframe breakups to the euphoric beauty of a carbon-fiber wing looping over open ocean waters. Underneath the technical post-mortems sits a poignant, reflective spirit marked by personal loss, ecological urgency, and an enduring pride in daring to pursue an audacious moonshot.
## Bulletin - [02:16](https://www.youtube.com/watch?v=qd_hEja6bzE&t=136s) Makani spent 13 years developing utility-scale airborne wind turbines, aiming to cut structural material by roughly 90% and cost from 20 cents to 3–4 cents per kilowatt-hour by replacing steel towers with tethered crosswind airfoils. - [01:10:25](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4225s) After scaling from the 20 kW Wing 7 prototype to the 600 kW M600 within Google X, the program demonstrated full autonomous flight cycles including vertical hover, crosswind generation, and robotic perch recovery. - [01:14:58](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4498s) Faced with plummeting land-based wind turbine costs, Makani pivoted offshore to deploy the M600 from a floating spar buoy in Norway, achieving crosswind generation over the North Sea before a trans-out crash in rough swells. - [01:38:41](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5921s) Despite proving crosswind flight physics and offshore feasibility, Makani shut down after spinning out from Alphabet when it could not secure commercial capital to fund multi-thousand-hour reliability testing.
## Key takeaways - [02:16](https://www.youtube.com/watch?v=qd_hEja6bzE&t=136s) Miles Loyd's 1980 crosswind aerodynamic theory showed that tethered airfoils sweeping across the wind harness far more power than stationary turbines while eliminating heavy ground towers. - [08:38](https://www.youtube.com/watch?v=qd_hEja6bzE&t=518s) Makani transitioned from commercial soft kites to rigid carbon-fiber airframes after early modeling proved rigid wings offered superior aerodynamic efficiency despite severe crash risks. - [14:20](https://www.youtube.com/watch?v=qd_hEja6bzE&t=860s) The 20 kW Wing 7 demonstrator proved the feasibility of autonomous vertical hover launch, tensioned crosswind loops, and perch docking. - [26:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1602s) Scaling 30x to the 600 kW M600 inside Google X drastically increased vehicle mass, tether line tension (peaking at 60–80 kN), and transition complexity. - [32:19](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1939s) To bypass severe delays in robotic ground station fabrication, engineers built 'Containerhenge' from stacked shipping containers to execute static 500-meter tether launches. - [54:32](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3272s) Energy kites operate without trim or steady-state equilibrium, combining glider-like high aspect ratios with continuous fighter-jet turning dynamics under tether tension. - [48:43](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2923s) 'Trans-out'—decelerating high-speed crosswind loops back into a stable hover—proved to be the most technically hazardous flight control challenge across all airframe generations. - [01:10:25](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4225s) Testing at Parker Ranch in Hawai'i validated full-cycle autonomous flight and robotic perching off a rotating ground station. - [01:14:58](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4498s) Rapid cost drops in conventional onshore wind forced Makani to pivot to deepwater offshore floating spar buoys in Norway, where traditional wind turbines are cost-prohibitive. - [01:31:14](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5474s) The North Sea demonstration achieved offshore launch and autonomous crosswind loops from a floating spar buoy, but dynamic buoy drift and tether slack led to an in-flight control divergence and water impact during trans-out. - [01:38:41](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5921s) Makani's commercial closure reflected the daunting moonshot capital gap: commercial viability demanded years of continuous runtime and multi-thousand-hour MTBF that private venture markets refused to fund. - [01:38:41](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5921s) Engineers compared Makani's trajectory to the 1940s Smith-Putnam wind turbine, demonstrating that pioneering energy architectures can validate foundational engineering long before the market conditions align.
## Detailed walkthrough ### [00:08](https://www.youtube.com/watch?v=qd_hEja6bzE&t=8s) The Audacity of Harnessing Wind with Kites
The endeavor to extract wind power using tethered wings demanded unprecedented engineering achievements across multiple disciplines simultaneously. As one team member explains, “It was heroic on a structural mechanics front. It was heroic on a materials science front. It was heroic on a power electronics front. It was heroic on an aerodynamics front. It was heroic on the control systems front.” The venture was a series of world firsts rather than standard aerospace engineering. Facing climate change as the defining problem of our time, the engineers were galvanized by the sheer audacity of trying to build something so open-ended.
```mermaid flowchart TD accTitle: Wind turbine tower versus Makani energy kite concept accDescr: Diagram contrasting conventional heavy wind turbines with Makani's lightweight tethered kite wing concept.
subgraph Traditional["Traditional Wind Turbine"] T1["Heavy Steel Tower & Foundation"] --> T2["Fixed Swept Area"] T2 --> T3["Expensive Scaling to Reach Better Wind"] end
subgraph Makani["Makani Energy Kite Concept"] M1["Lightweight Tethered Airfoil"] --> M2["Sweeps Large Crosswind Area"] M2 --> M3["Generators Onboard Free Wing"] M3 --> M4["90% Less Material at Lower Cost"] end ```
The team’s initial flight logbooks reflected both the ambition and the brutal trial-and-error nature of the early work. After tallying a modest milestone of five minutes of autonomous flight, the tally also stood at “four dead kites.” Instead of designing incremental improvements to standard wind turbines, Makani was fundamentally asking what the most optimal system possible would look like to extract wind energy, and then attempting to build that from the ground up.
[02:16](https://www.youtube.com/watch?v=qd_hEja6bzE&t=136s) Origins, Economics, and the Physics of Crosswind Flight
In late 2006, the narrator joined Makani Power as the company archivist to chronicle the mission. Earlier that year, a group of engineers and avid kiteboarders began experimenting with airfoils. Their time on the water had given them a visceral understanding of wind energy, leading them to ask whether heavy steel turbine towers could be discarded in favor of a lightweight, tethered airfoil.
The economic backdrop of 2006 made the concept intensely appealing. Before the boom in hydraulic fracturing made natural gas cheap, wind energy sat at roughly 20 cents per kilowatt-hour. A back-of-the-napkin calculation convinced Makani's founders they could generate electricity for three to four cents per kilowatt-hour—or even cheaper if things broke their way.
The foundational physics originated in a 1980 paper by Miles Loyd. Loyd demonstrated that a kite flying dynamically across the wind sweeps a far greater cross-sectional area of sky and generates substantially more power per unit of time than a turbine locked in a single spot.
- **Miles Loyd's 1980 principle**: A tethered wing flying crosswind acts like the tip of a giant wind turbine blade, but without the physical tower holding it up. - **Sailboat dynamics**: Just as a sailboat redirects wind to create forward drive and sideways heel, a crosswind kite redirects airflow into forward motion, pulling against its tether to turn onboard generators. - **Material savings**: By replacing the structural steel tower with a high-strength tether and using a lightweight aerodynamic wing with onboard rotors, the system aimed to access stronger, higher-altitude winds while using roughly 90% less material.
[08:38](https://www.youtube.com/watch?v=qd_hEja6bzE&t=518s) Soft Kites to Rigid Wings: The 2.6-Second Crash
Makani began testing with commercial soft kites—essentially large kiteboarding kites—generating electricity on the ground through a mechanical winch. This setup allowed cheap, rapid iteration, embracing the rule that “you can only learn so much from simulations. At some point, you just really have to interact with reality.” Analytical models, however, soon indicated that rigid wings would yield far higher energy generation efficiency.
Pivoting away from their rapid prototyping ethos, the team spent nine full months designing and constructing a complex, carbon-fiber rigid wing based almost entirely on simulations. Because they only built a single prototype, they had zero margin for error. After tethering it for safety checks in Santa Cruz, they initiated flight:
> “Two point six seconds of flight.”
The nine-month carbon-fiber prototype slammed into the earth and splintered. The crash was a crushing blow, but it delivered a crucial lesson about the dangers of over-relying on simulations without real-world feedback.
```mermaid flowchart LR accTitle: Evolution of early Makani kite architectures accDescr: Three early prototyping stages from soft kites to the overbuilt carbon wing, leading to the Wing 6 breakthrough.
A["Soft Kites & Ground Winch<br>(Fast iteration, low efficiency)"] --> B["First Rigid Carbon Wing<br>(9 months to build; crashed in 2.6s)"] B --> C["Hackable Rigid Wing 6<br>(Styrofoam, tape, guy wires)"] C --> D["Successful Hover & Crosswind Transitions"] ```
[10:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=642s) Wing 6 and the Culture of the Shop
Anticipating that the expensive carbon prototype might fail, part of the team had simultaneously assembled a cheap, bare-bones backup wing. The day after the nine-month carbon kite shattered, they took this cheap wing to the field, and it flew steady loops. That immediate success validated the rigid crosswind concept and led directly to Wing 6: an unglamorous, hacky aircraft cobbled together from styrofoam, guy wires, and tape. Wing 6 was specifically designed to tackle the hardest aerodynamic problem yet: launching vertically in a hover, pitching forward into autonomous crosswind power-generation loops, and transitioning back to a hover for recovery. Against its awkward looks, Wing 6 nailed the transitions cleanly.
The technical breakthrough was rooted in the unique shop culture at Makani, where long hours were set to blasting music and shared coffee:
> “My name is Tommaso Romanelli, I want to work here.”
- **Munho**: A master craftsman from Korea who had previously constructed and flown his own experimental composite airplanes before joining Makani. - **Tommaso Romanelli**: An Italian engineer and fabricator who heard about Makani's fight against climate change, flew to San Francisco, attended language school to learn English (where he met his future wife, Anita, who also joined Makani), and arrived at the door demanding a job. - **Shop environment**: Tommaso worked with disposable blue nitrile gloves covered in handwritten Sharpie notes, scribbling down slang, song lyrics, and English idioms—such as asking his colleagues, “Professor what's another name for pirate treasure?”—blending mechanical craft and human connection.
[14:20](https://www.youtube.com/watch?v=qd_hEja6bzE&t=860s) Building Wing 7 and Scaling Beyond Quick Iterations
After years of rapid iteration with inexpensive materials, Makani reached a configuration that proved the basic physics of airborne wind energy. Translating the abstract concept of combating climate change into a tangible machine brought the team closer together, creating deep bonds that went far beyond mere colleagues. To transition from a scrappy proof-of-concept into a commercial-grade product, the team needed to build an airframe capable of handling substantial operational stresses. This led to Wing 7, a rigid airframe designed to mount rotors and onboard generators to execute hover launch, crosswind power generation, and landing, with a rated output of 20 kilowatts.
```mermaid flowchart TD accTitle: Wing 7 Key Subsystems and Flight Roles accDescr: Diagram showing how Wing 7 components support launch, flight, and power generation.
subgraph Airframe ["Wing 7 Carbon Airframe"] CF["Carbon Fiber Structure"] Rotors["Onboard Rotors & Generators (20 kW)"] end
subgraph TetherSys ["Ground Connection"] Teth["Tether Line"] Constraints["Safety Constraint Line (Early Tests)"] end
subgraph Ops ["Operational Roles"] Hov["Quadcopter Hover Launch & Land"] Cross["Crosswind Loops (Power Generation)"] end
CF --- Rotors Rotors --> Hov Rotors --> Cross Teth --- CF Constraints -.->|"Initial Envelope Expansion"| CF ```
Building Wing 7 meant revisiting carbon fiber construction—a high-stakes, expensive, and time-intensive manufacturing method the team had avoided ever since destroying their first carbon prototype in a crash. Backed by fixed-term funding from the U.S. Department of Energy and Google.org, as well as extensive empirical flight data, they committed to carbon composites to withstand higher flight loads. Before allowing the wing to fly untethered in open airspace, the team took extreme precautions by testing it under safety constraint lines to verify that the control software and mechanical subsystems functioned harmoniously. Controlling a rigid aerodynamic craft acting simultaneously as a tethered kite and an autonomous quadcopter presented dynamics no aerospace engineers had ever previously resolved.
- Wing 7 was engineered to produce 20 kilowatts of electrical power while proving every commercial flight mode. - Funding was secured from Google.org and the U.S. Department of Energy (ARPA-E). - Runway assembly was celebrated as a milestone: “Historic? This is the first first ever assembly on the runway.” - Engineers treated the first untethered outing with dry reverence: “Wing 7, may you return to the ground in one piece.”
---
[16:10](https://www.youtube.com/watch?v=qd_hEja6bzE&t=970s) The First Free Flight and "Trans Out"
Eventually, safety constraints could yield no further actionable engineering data, forcing the team to commit to free flight. Because an errant tethered wing could sweep across the ground within seconds, the crew maintained strict emergency protocols, assigning safety cover positions behind vehicles and testing emergency stop routines. With six-meter-per-second winds confirmed and launch lines burned through, Wing 7 lifted into an autonomous hover ten meters above a support fire truck before pivoting forward into tensioned crosswind loops.
```mermaid flowchart LR accTitle: Wing 7 Flight Profile accDescr: Linear flow of the early Wing 7 test flight envelope.
Launch["Hover Launch (Quadcopter)"] --> Tension["Tension Line & Accelerate"] Tension --> Crosswind["Crosswind Loops (Power Generation)"] Crosswind --> TransOut["Trans Out (Crosswind to Hover)"] TransOut --> Landing["Glide Landing (Tether Release)"] ```
The flight proved aerodynamically chaotic as the tether continuously changed load angles. The most critical controls hurdle was "Trans Out"—transitioning the high-speed craft out of crosswind figure-eights back into a stationary hover. In early flight runs, once Trans Out succeeded, the ground crew released the tether completely, pitching the wing downward into an unpowered glide landing on the runway grass.
> “It looks like an airplane. It's not an airplane. It's an airplane with a string that changes directions constantly. Nothing's ever still nothing's ever steady.”
> “I think it takes one part bravery and one part blind optimism to keep your prototype in the air when your flight looks this bad.”
---
[19:25](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1165s) Field Cadence, "Flangry" Engineers, and the Loss of Corwin Hardham
Field operations quickly settled into a grueling cycle governed by unpredictable weather and tight daylight windows. The team found themselves stranded on dry lake beds and airfields either waiting for dead calms to pick up or battening down equipment when winds blew past operating limits. Long, exhausting setup times and natural wildlife encounters—such as mistaking a harmless gopher for a baby rattlesnake—punctuated long days of troubleshooting overheated motors and rewriting flight controller code.
```mermaid flowchart LR accTitle: Field Testing Iteration Loop accDescr: Cycle of testing, hardware failures, and software iterations.
Setup["Rig Field Site"] --> Launch["Flight Test"] Launch --> Failure["Component Breakdown / Overheating"] Failure --> Analysis["Diagnose Weak Points"] Analysis --> Patch["Patch Code & Swap Motors"] Patch --> Setup ```
To describe the specific tension that gripped the engineering team when technical setbacks or calm weather kept the wing grounded for weeks, they coined the term "flangry"—an anxious hunger for flight testing and forward momentum. Progress was steady but incremental, until tragedy struck the team: Corwin Hardham, Makani's CEO and co-founder, passed away suddenly and unexpectedly. Hardham had served as the cultural and operational bedrock of the company, doing everything from setting attainable technical milestones to baking fresh bread and making lunch for the crew. Propelled by his memory, the team resolved to push the technology forward without hesitation.
> “Around this time, we coined the term flangry, which is how we'd feel when we hadn't flown in a long time. This kind of anxious hunger for progress.”
> “It had always been clear that Corwin was driven to make Makani succeed as a part of the way he cared for people and the environment.”
---
[22:12](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1332s) Conquering "All Modes" and Autonomous Perching
Honoring Corwin Hardham’s vision meant tackling the ultimate systems engineering hurdle: demonstrating "All Modes" in a single automated flight cycle. Up to this point, the kite had been developed to fly independently of the ground station, while landings required unlatching the tether for manual glide recoveries. The complete commercial concept required a specialized robotic ground perch to physically catch the incoming kite vertically, manage high-speed winching across every flight regime, and route electrical current bi-directionally along the tether.
```mermaid flowchart LR accTitle: Autonomous Perch All Modes Cycle accDescr: Complete loop of autonomous perch takeoff, crosswind loops, and perch recovery.
PerchHold["Perched on Ground Station"] --> AutoLaunch["Vertical Hover Launch"] AutoLaunch --> TransIn["Trans In: Accelerate to Tension"] TransIn --> Generating["Crosswind Power Loops (5-6 kN)"] Generating --> TransOut["Trans Out: Decelerate to Hover"] TransOut --> AutoPerch["Vertical Docking onto Ground Station"] AutoPerch --> PerchHold ```
Combining the airborne kite and the dynamic ground station created an intricate control problem. On test day, the flight priorities were starkly prioritized: avoiding a crash was goal number one, followed by automated perch takeoff and landing, executing crosswind in the middle, and finally, generating power. During the flight, Wing 7 smoothly executed "Trans In," reeled out into full crosswind generation pulling line tensions between 5,000 and 6,000 Newtons, initiated "Trans Out" despite sharp roll maneuvers, and backed itself onto the perch needles to lock down successfully. The team celebrated this world-first achievement with plans for extended endurance testing.
- The ground station managed three vital roles: serving as a mechanical perch, controlling tether deployment and tension, and transferring electrical power to and from the grid. - Tension readings held steady at 5,000 to 6,000 Newtons through the circular flight path before retrieval. - Ground crews were ecstatic after autonomous docking: “Yes! Sick! Next we're flying for 10 hours, 10 hours of awesome.” - One engineer reflected on the milestone: “Working on something hard for a long time as part of a team and watching it work exactly as you'd intended it to is as good as it gets.”
---
[26:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1602s) Joining Google X and Scaling to the 600-Kilowatt Kite
Proving the multi-mode autonomous flight cycle confirmed that airborne wind was technically feasible, shifting Makani’s focus to long-duration endurance runs. Pushing the prototype toward ten continuous operational hours uncovered critical real-world failure modes—such as motor thermal limits and complex differential aerodynamic drag behaviors—that simulations failed to capture. However, Makani's leadership knew that a 20-kilowatt platform was merely a technology demonstrator. Generating utility-scale power to meaningfully replace fossil fuels demanded a machine thirty times larger.
```mermaid flowchart LR accTitle: Scale Comparison Between Wing 7 and Commercial Prototype accDescr: Scale jump from the 20 kW Wing 7 demonstrator to the 600 kW utility system.
subgraph W7 ["Wing 7 Demonstrator"] W7P["20 kW Rated Power"] W7S["Subscale Testbed"] end
subgraph W600 ["Utility-Scale Moonshot"] W600P["600 kW Rated Power"] W600S["~300 U.S. Homes Powered"] W600X["Integrated into Google X"] end
W7 -->|"Scale Factor: 30x"| W600 ```
To build a full-scale machine, Makani joined Google X (the moonshot factory), securing the capital and engineering infrastructure necessary to construct a 600-kilowatt airborne wind turbine capable of powering roughly 300 homes. The team spent over a year working through grueling design challenges for the massive composite airframe and high-voltage power electronics. Transitioning between flight modes became exponentially more dangerous as the mass, wingspan, and tether line forces jumped by orders of magnitude, turning routine design obstacles into towering engineering barriers.
> “At X we would have the resources we needed to scale up to a utility sized kite that would get us closer to expanding access to renewable energy for billions of people around the globe.”
> “I don't know if hurdle is the right word when the hurdle is three meters high it's not a hurdle anymore, but we kept on going at it.”
[29:57](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1797s) Continuous Integration and Ground Station Roadblocks
Transitioning from the small-scale Wing 7 to Makani's first utility-scale energy kite felt surreal to the crew standing beneath it. Visually, the new airframe appeared identical to Wing 7, only enormous, making the team members look miniature beside it. Rather than waiting for a fully realized aircraft before beginning flight tests, the team adopted an aggressive, incremental strategy. The earliest iterations were tested without flaps, aileron servos, a tail, or an empennage. The team took to the field with what was admittedly the wrong wing, the wrong motors, and an incomplete ground power system, trusting that anything sufficiently representative would yield vital operational knowledge.
```mermaid flowchart TD accTitle: Incremental Kite Development and Testing Bottleneck accDescr: Flowchart illustrating the year and a half of continuous hardware integration leading to ground station redesign and the Containerhenge workaround.
subgraph Integration ["Iterative Kite Testing (1.5 Years)"] A["Incomplete Wing Assembly"] --> B["Integrate Flight Motors"] B --> C["Install New Ground Inverter"] C --> D["Hover Testing Under Constraints"] end
subgraph Bottleneck ["Ground Station Failure"] D --> E{"Assess Scaled-Up Ground Station"} E -->|"Multiple Failures"| F["Full Redesign Needed (1 Year Delay)"] end
subgraph Workaround ["Parallel Fast-Track"] F --> G["Design Next-Gen Ground Station"] F --> H["Build 'Containerhenge' Perch"] H --> I["Immediate Crosswind Flight at China Lake"] end ```
For a year and a half, Makani maintained a continuous loop of integration and tethered hover tests. Whenever upgraded hardware arrived, engineers swapped components and returned immediately to the test pad: when long-awaited flight-grade motors were delivered, the crew spent two weeks retrofitting them before resuming testing; when upgraded ground inverters arrived, they were dropped into the loop. Reflecting on this grueling phase, the team recognized that attempting a traditional aerospace waterfall rollout would have doomed the initiative: “I think if you had tried to complete the system and then put it together, there was no way you would get it to go.”
By the end of this integration campaign, the kite was hovering reliably on constraints, but the ground station presented an existential roadblock. Multiple severe mechanical and electrical issues emerged on the scaled-up ground winch and perch system. A proper redesign and rebuild of the ground station would consume the better part of a year—time the program did not possess. Funders, internal milestones, and the urgency of the climate mission demanded that the team prove crosswind power generation immediately rather than spend twelve months refining ground support hardware.
- The first iteration tested lacked fundamental flight control surfaces, including aileron servos, flaps, and a tail empennage. - Continuous hover and integration cycles spanned roughly 18 months before crosswind testing was attempted. - Redesigning the full automated ground station threatened to delay the flight program by nearly a year.
---
[32:19](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1939s) Team Jargon and the Birth of Containerhenge
To keep morale high and streamline daily operations, the Makani crew developed an idiosyncratic internal vocabulary. Hardware, safety protocols, and maneuvers were frequently named after the colleagues who conceived them. When the company found itself employing four different men named Jeff, the roster was parsed into Geoff, Rocket Jeff, Laser Jeff, and Just Jeff. When Rocket Jeff engineered an electronics enclosure for the M600 kite, it was permanently christened the "rocket box." Even when the component malfunctioned in the field, the crew regarded it fondly simply because everyone loved Rocket. Similarly, an automated maneuver that stepped the tethered kite safely to the right so personnel could walk across the flight pad was officially dubbed "the Nicholas," named after the engineer who devised and coded the routine.
Faced with a stalled ground station development timeline, the team applied this same improvisational mindset to build a rapid workaround: "Containerhenge." Rather than waiting on a motorized winch drum and gimbal system, engineers stacked standard steel shipping containers into two side-by-side towers. This static remote perch held the kite aloft at the full 500-meter tether length, completely bypassing the complex reeling and tensioning mechanics required for spooling the tether in and out during launch.
Containerhenge was engineered with pragmatic, low-cost modifications: - **Perch Pegs:** Specialized load-bearing pegs were retrofitted onto the kite to distribute the wing's resting weight evenly across the two container stacks. - **Platform Netting:** Heavy-duty nets were secured across the top surfaces of the containers, giving ground crews a visual reference for wing alignment while generating friction to keep the kite from being dragged forward by the tension of the 500-meter tether. - **Tail Spike and Arrestor Cables:** To prevent the tall kite from pitching forward off the perch before motor thrust engaged, a tail spike was added to catch across two tensioned cables strung across the central gap between the container stacks.
---
[34:04](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2044s) SN2, the Birdcage, and Existential Stakes
With Containerhenge standing, the operational focus shifted from the Serial Number 1 (SN1) hover test rig to Serial Number 2 (SN2), Makani's first fully crosswind-capable kite. While SN1 spent a year enduring constrained hover flights, SN2 was finalized inside the "Birdcage"—Makani's hangar and assembly facility—where engineers conducted spinning motor checkouts. Rolling SN2 out of the Birdcage marked the penultimate milestone before packing the flight program for China Lake, a sprawling military test range in the California desert large enough to accommodate full-circle crosswind flight at maximum tether extension.
The transition was shadowed by extreme organizational pressure. Before leadership would authorize the logistical move to the desert, SN2 was required to complete 16 cumulative hours of hover testing to prove its mechanical and avionics reliability. Makani was operating under a strict year-end deadline: if the team failed to relocate to China Lake and demonstrate autonomous crosswind flight before the calendar ran out, the project faced drastic budget reductions or outright cancellation by parent company Alphabet.
Early in SN2's 16-hour qualification regime, unexpected technical gremlins surfaced. Most alarming was an unforeseen structural resonance: when the wing's eight electric motors spun up to specific operating frequencies, the motor pylons began vibrating violently. Control engineers scrambled to damp out the oscillation through software, resorting to a blunt approach: “Ah, we just lower gains. We just keep lowering gains.”
- SN1 was dedicated exclusively to hover envelope expansion, while SN2 was built to withstand the aerodynamic forces of crosswind loops. - China Lake provided the vast restricted airspace needed to fly an energy kite tethered to a 500-meter line without civilian aviation interference. - The project faced potential termination if crosswind flight was not demonstrated before the end of the year.
---
[36:05](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2165s) Debugging Motor Faults and Calculating Risk
As SN2 neared the final hours of its mandatory 16-hour hover qualification, the flight line descended into an exhausting game of troubleshooting. During one tethered hover, an abrupt motor controller fault caused the kite to lose lift instantly and drop hard onto its safety constraints. Ground cameras caught the sudden fall as crew members called out the drop in shock. Engineers traced and patched the fault, only to encounter an entirely different failure on the very next test: the starboard bottom outboard (SBO) motor refused to spin up at launch.
The SBO motor anomaly remained unexplained, presenting the leadership team with a difficult tactical dilemma. The 16-hour hover requirement had technically been satisfied late on a Friday, but the aircraft harbored a persistent, undiagnosed intermittent bug. Canceling the desert deployment would allow thorough bench testing in the Birdcage, but would forfeit the scheduled range reservation at China Lake and ensure missing the year-end crosswind milestone. Conversely, deploying with a known glitch risked crashing Makani's only crosswind airframe during its maiden launch.
Inside the team, engineers debated the fine balance between flight test caution and the necessity of real-world operational tempo. Ultimately, leadership decided to proceed with the logistics convoy while holding the wing back for last-minute bench checks if needed. The overarching philosophy favored bold operational testing over ground paralysis: “Like your chances of learning, which is, was, always really our objective, are higher if you assume the risk and fly.”
- A sudden motor controller fault caused an uncommanded drop onto pad constraints during hover trials. - The starboard bottom outboard (SBO) motor experienced intermittent ignition failures of unknown origin right before deployment. - Range reservations, logistical commitments, and existential deadlines prompted the team to accept the residual motor risk and ship to China Lake.
---
[39:15](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2355s) Operations at China Lake and the Perch Mishap
Arriving at the desert expanse of China Lake, the crew was greeted by blistering sun, rugged dry lakebeds, and high spirits. Initial shakedown flights went smoothly; an initial flight lasting one hour and ten minutes, paired with a subsequent short hop, fulfilled the 75 minutes of baseline hovering required before transitioning to the heavy tether. Despite erratic winds blowing from unideal directions, the flight controllers maintained stable hover authority. The crew celebrated under the desert sun, trading jokes about their developing farmer tans and marveling at the crane operators maneuvering heavy hardware across the pad.
```mermaid flowchart LR accTitle: Unconstrained Flight Sequence and Emergency Wing Save accDescr: Sequence diagram tracing the perch repair, Containerhenge launch, tether failure, and manual emergency landing.
subgraph LaunchPrep ["Pad Prep & Field Repair"] A["Perch Peg Collapses Overnight"] --> B["Rivet Trailing Edge in Field"] B --> C["Hoist to Containerhenge Perch"] end
subgraph Flight ["Launch & Transition"] C --> D["Unconstrained Launch"] D --> E["Ascend to 11m Above Perch"] E --> F["Transition into Crosswind Loop"] end
subgraph Recovery ["Emergency Recovery"] F --> G{"Tether Break!"} G --> H["Pilot Declares 'Wing Save'"] H --> I["Manual Rudder & Flare Control"] I --> J["Belly Landing with 4 Pylons Intact"] end ```
The mood shifted abruptly the following morning. The kite—spanning the wingspan of a small transport aircraft—had been hoisted onto the Containerhenge perch the night before, awaiting only routine mechanical pre-flight checks before flying unconstrained without safety ropes for the first time. Overnight, shifting winds had caused the kite to settle awkwardly on the perch. The localized load crushed one of the perch pegs, driving the airframe downward and splitting the composite trailing edge of the wing.
The damage threatened to halt the campaign. Performing a standard composite wet-layup repair and waiting for structural epoxy to cure would exhaust the test window, prompting an engineer to state plainly: “To fix this, is to fly next year.” Unwilling to forfeit their shot at crosswind flight, the team executed an expedient field repair. Technicians replaced the crushed perch-peg tip, aligned the torn composite skin, and blind-riveted the trailing edge together directly on the pad.
- Flight crews completed a 1-hour-and-10-minute shakedown flight in desert winds to certify flight systems for the heavy tether. - The kite airframe was comparable in span to a commercial airliner, flying without tethers or tethers limited by safety cranes for the first time. - Overnight movement cracked the trailing edge of the carbon wing, prompting an emergency field fix using rivets rather than structural composite curing.
---
[42:14](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2534s) The First Unconstrained Crosswind Flight and Tether Break
Launching off Containerhenge presented razor-thin margins of error. The kite sat perched atop rigid steel shipping containers that offered zero forgiving clearance: any wind gust pushing the aircraft sideways during liftoff risked smashing the wing against the structures. Furthermore, because Containerhenge was fixed in place, successful departure required the desert wind to align precisely with the launch axis. As telemetry ticked past eleven meters of altitude, the flight controller confirmed that the port perch peg was light, the bridle cleared, and the kite ascended smoothly into the sky.
The aircraft pushed forward into "trans-in"—the high-risk transition phase where the kite pitches down from a stationary vertical hover, builds airspeed, and enters high-speed circular crosswind loops. To the cheers of the control room, the kite carved through the air and began its turn, with flight controllers confirming: “Crosswind normal, we're in crosswind.” For a brief few seconds, Makani had achieved utility-scale airborne crosswind flight.
Disaster struck instantly afterward. The tether snapped, severing the physical and electrical connection between the kite and the ground: > “We lost the tether, we lost the tether, lost the tether.”
With ground power and tether tension gone, the automated crosswind control loop collapsed. A human pilot instantly engaged manual override, calling out “Wing save!” over the radio net to execute emergency unpowered glide protocols. Flight controllers tracked telemetry through secondary radio links, calling out headings, aggressive left-rudder inputs, and flare commands as the glide path degraded. Fighting to clear the ground infrastructure and orient the wing into the wind, the pilot flared just above the desert floor, guiding the multimillion-dollar prototype into an emergency belly landing. The kite skidded across the dirt with all four motor pylons intact. Though the tether had failed, the crew celebrated the wing save as a monumental partial victory: the kite had survived launch, flown crosswind, and proved that its airframe could be manually recovered from a catastrophic mid-air disconnect.
- The kite successfully launched unconstrained, climbed past 11 meters, and initiated autonomous transition into crosswind loops. - A sudden tether failure severed kite power and structural line tension seconds after crosswind entry. - The manual "wing save" protocol allowed pilots to glide the aircraft away from Containerhenge and land flat in the desert with the pylons and wing structure largely intact. - The deployment verified testing between two competing tether architectures: a solid carbon fiber core design versus a multi-strand carbon core.
[45:35](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2735s) Stranded Core Tether and the First Crosswind Loop
Although the lighter solid-core tether had shown promise in laboratory testing, it failed immediately in the field before Makani could execute a single crosswind loop. While the failure provided valuable empirical data, the team understood that failed experiments would not keep the program alive; they had to demonstrate crosswind flight to guarantee continued backing. Fortunately, an alternative stranded-core tether was already prepared. After patching the damaged trailing edge of the wing and spooling out the stranded-core line, the ground crew prepared for another attempt despite an unpromising wind forecast. Facing marginal breeze conditions, the crew debated whether to hold back or commit. Acknowledging their nervousness—yet recognizing the fleeting window of opportunity—they decided to push forward.
The launch team initiated throttle, calling out wind speeds climbing through seven and nine meters per second as the kite lifted into ascend mode. Control callouts tracked every critical parameter as motor gains ramped, the tail cleared the ground perch, and the vehicle threaded the narrow clearance corridor above the safety nets. Reaching an altitude of 21 meters, the kite stabilized in full-length hover, translated to the target azimuth, and accelerated into "trans-in" along the spherical tether boundary. Slipping smoothly into crosswind flight under 30 kilonewtons of line tension, the wing traced circular paths across the sky, with the detwist mechanism tracking the rotations. As the kite swept past nine o'clock and completed its very first loop, someone over the radio exclaimed, “Happy New Year everybody.” Reaching top speeds of 35 meters per second and climbing over the loop apex at 30 meters per second, observers noted that tether current appeared to reverse—the earliest tangible sign that the airborne turbine was generating electrical power back down the line.
- Solid-core tether failed prior to completing the first crosswind loop; replaced immediately with the backup stranded-core tether. - Launch occurred in light winds (forecast showed little wind until late in the day), ascending to hover at 21 meters altitude. - Tether line tension reached 30 to 31 kN at bottom of loop, peaking between 60 and 80 kN over the top. - Flight speeds during circular loops ranged between 30 and 35 meters per second.
```mermaid flowchart TD accTitle: Makani Flight Regimes and Transitions accDescr: Flowchart illustrating the primary flight states from launch through crosswind power generation, perch landing, and emergency autoglide.
subgraph Launch["Launch Phase"] A["Ground Perch"] --> B["Vertical Hover & Ascend"] B --> C["Hover Full Length at Azimuth"] end
subgraph Crosswind["Power Generation Cycle"] C -->|"Accel & Trans-In"| D["Crosswind Flight (Loops)"] D -->|"Circular Aerodynamic Orbit"| D end
subgraph Recovery["Recovery & Landing"] D -->|"Trans-Out (Deceleration & Turn)"| E["Hover Translation"] E -->|"Descend"| F["Perch Capture & Latch"] D -.->|"Emergency MV Loss / Tether Cut"| G["Deadstick Autoglide Landing"] end ```
---
[48:43](https://www.youtube.com/watch?v=qd_hEja6bzE&t=2923s) Trans-Out Dynamics and the Control Law Dilemma
Successfully entering crosswind flight solved only half the aerodynamic problem; the vehicle still had to safely exit crosswind and return to a stationary hover. While both pure hover and pure crosswind flight were well understood, the transition between them—termed "trans-out"—represented uncharted territory. In crosswind, the kite behaved like a high-speed glider flying circular tracks while extracting energy from the wind. Transitioning out required shedding that kinetic energy almost instantly, transforming the craft from a passive aerodynamic generator into an active, power-consuming multi-rotor hover platform while simultaneously completing a directional turn.
During early trans-out testing, the kite pitched violently backwards as high winds pushed it downwind. The craft began descending at an alarming rate, rolling up to 50 degrees in gusts measuring 10 meters per second. Control room monitors watched the telemetry plummet from 60 meters down toward 30 meters, prompting exclamations of terror as the sagging tether hit the ground. The kite autonomously arrested its plunge just 20 meters above the desert floor. Reviewing the telemetry, engineers realized the physics of the tethered kite defied classical aerospace design assumptions: “From a control laws perspective you can't just be a traditional control law designer here and apply the same old airplane feedback that you do anywhere else.” The machine was fundamentally different, demanding entirely new control algorithms designed to handle coupled aerodynamic, mechanical, and tether dynamics.
- Hovering and circular crosswind flight were mature concepts, but simultaneous deceleration, vehicle rotation, and mode-switching during trans-out were unprecedented. - During an uncontrolled sink event after trans-out, roll angles reached 35 to 50 degrees under 10 m/s winds from 60 degrees. - Vehicle descended rapidly to 20 meters above ground level with the tether touching the dirt before the flight controller recovered hover stability.
---
[50:54](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3054s) Broken Tailspikes and Emergency Autoglide Landings
Landing operations presented severe physical constraints. The desert test site was optimized for a specific prevailing wind corridor; whenever the wind shifted off-axis, the kite had to fight crosswinds while descending into a narrow footprint bordered by heavy shipping containers. In one recovery attempt, turbulent gusts induced unstable roll oscillations from -10 to -14 degrees as the pilot tried to hover into position. During the approach, an unexpected mechanical failure struck: the tailspike—the critical structural element required to dock and latch onto the ground perch—sheared off completely. Without it, any perch touchdown would result in the nose pitching directly forward into a destructive faceplant.
Faced with a compromised vehicle, the team elected to climb back into ascend mode, throttle up, and transition once again into crosswind flight to climb to safe release altitude. After banking through a series of left-hand circular turns past six, nine, and twelve o'clock, the command was issued at two o'clock to sever the tether. With release confirmed, the kite entered autoglide mode at an altitude of 270 meters. Johnny piloted the unpowered aircraft on manual deadstick approach, coordinating rudder adjustments to keep the wings level through 40, 30, and 20 meters before initiating a landing flare at seven meters. The kite touched down smoothly on the desert floor, prompting an enthusiastic reaction from mission control: “Johnny that was f*ing fantastic.” Demonstrating successful unpowered glide recovery was a monumental achievement for airborne wind energy and proved decisive in convincing X to extend funding.
- Landing approach corridor was constrained by large metal shipping containers and sensitive to shifting wind vectors. - Shearing of the tailspike eliminated the possibility of a normal perch landing, forcing the team to re-climb to 270 meters for an intentional release. - Successful unpowered deadstick autoglide touchdown proved the kite could survive complete tether disconnection or power failure. - Flight proved Makani could control an airborne structure the size of a commercial wind turbine blade, securing continued support from X.
---
[54:32](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3272s) The Iterative Flight Cycle: Glider Body, Fighter Jet Turns
With continued funding secured, the Makani engineering team settled into an intensive iterative development rhythm: fly, pull the telemetry logs, identify discrepancies between reality and simulation, refine the software and physical flight parameters, and return to the flight line. Early data showed that the physical kite did not track designated flight paths with the precision modeled in software, and its nose angle relative to the incoming wind vector exhibited minor offsets. By testing corrections in simulation before validating them in live flights, the team methodically smoothed vehicle behavior. Pre-flight morning briefings combined rigorous procedural rehearsals, hardware checks, and long waits for ideal wind windows, targeting two-hour continuous flight profiles culminating in perch landings.
The aerodynamic reality of the Makani platform created an extreme challenge for control theory. Normal aircraft fly straight toward a waypoint or trim out to an equilibrium state where flight sensors can collect baseline measurements. The energy kite, by contrast, operated in perpetual dynamic instability: constantly rolling, accelerating, pulling high-g turns, and changing velocity along its circular trajectory. As one engineer described the machine’s contradictory physical nature: “I can't think of vehicles that fly like this. We're shaped like a glider. We're making turns like a fighter jet. It's an unusual machine.” Despite having no steady-state flight condition to anchor their algorithms, the controls team steadily improved the smoothness of crosswind power loops and trans-in/trans-out transitions.
- Development cycle operated on an iterative loop: flight data collection, simulation reconciliation, control adjustments, and live re-testing. - Crosswind flight never reaches an equilibrium or trim state, requiring constant high-rate maneuvering, variable airspeed, and continuous acceleration. - Vehicle geometry balanced high-aspect-ratio glider aerodynamics with high-agility fighter aircraft turn dynamics on a high-tension line.
---
[58:18](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3498s) Ground Power Trip, BMX Wheel Touchdown, and Redefining Success
During an otherwise promising endurance flight, an unexpected electrical fault abruptly interrupted testing. A rapid surge of onboard power generation back-fed into the ground station grid, overwhelming the ground power equipment and triggering a uninterruptible power supply (UPS) alarm. Interpreting the sudden spike as a fault, the ground generator automatically shut down power transmission up the tether, causing an immediate loss of motor voltage (MV) on the wing. With no propulsion available to maintain flight on the tether, the crew immediately triggered the tether release at 98 meters while traveling 33 meters per second.
The kite glided down rapidly through 40 meters at 21 meters per second, touching down on the dirt and pitching forward into the ground. While the unpowered touchdown crumpled the forward nose assembly, the lightweight landing gear absorbed the brunt of the kinetic energy, successfully saving the composite tail surfaces and primary wing box from catastrophic destruction. Reviewing the wreckage, the landing gear's mechanical engineer noted the extreme design trade-offs involved: “I mean, we are trying to land something that weighs as much as a car on two BMX wheels.” While the landing was far from pristine, the team recognized that taking enough kinetic energy out of the crash to preserve critical structures represented real success. The team resolved the electrical protection issue on the ground and repaired the wing, but manufacturing lead times forced them to wait months for a replacement tether before flying again on the one-year anniversary of their first crosswind loops.
- An onboard electrical generation surge overloaded the ground power system, triggering protective shutdowns that cut high-voltage power to the kite motors. - Kite was released from the tether at 98 meters altitude while traveling at 33 m/s, touching down at 21 m/s. - Custom landing gear utilized two BMX bicycle wheels designed for a very narrow landing window, carrying an aircraft weighing as much as an automobile. - Landing gear designer had explicitly assigned only a 60% probability of success to the narrow-envelope landing system. - Structural sacrifice of the nose and landing gear successfully prevented total roll-over and protected the tail assembly and main wing. - Ground power protection systems and airframe repairs were resolved, though tether replacement took several months to fabricate and deliver.
[01:01:20](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3680s) RPX-08 Success and the Long Game of Moonshot Technology
The team endures the grinding cycle familiar to experimental flight testing: setting up hardware, waiting on the weather, packing everything back down, and starting all over again in hopes that “the wind gods come today.” Flight test RPX-08—jokingly dubbed “take three... or like two point five”—finally gets its window. As the kite descends toward the perch, operators carefully guide the touchdown in tense real-time callouts: five meters, four, three, starboard wingtip close, down to one meter, tailspike aligning, sliding slightly to port, and finally settling securely on the ground.
```mermaid flowchart LR accTitle: RPX-08 to RPX-09 Flight Progression accDescr: Sequence showing setup, successful flight RPX-08, and the mid-air breakup of RPX-09 leading to root cause analysis. subgraph S1["Flight RPX-08"] A["Setup & Weather Holds"] --> B["Successful All-Modes Test"] B --> C["Safe Touchdown on Perch"] end subgraph S2["Flight RPX-09 Incident"] C --> D["RPX-09 Flight Launch"] D --> E["In-Flight Breakup & Crash"] E --> F["Root-Cause Flight Data Analysis"] end ```
The flight caps a watershed year. The engineering milestones have systematically eliminated the early doubts that dog ambitious hardware ventures: - The team dismantled criticisms like “they're flying but they're not making any power” or “they have a machine, but they're not flying yet.” - They proved the core product works: generating utility power reliably, completing repeated flights, and recovering gracefully from flight errors. - Yet building entirely new physical architecture remains a grueling commercial challenge: “And so to accumulate the adequate degree of experience and reliability and be able to demonstrate to investors that the system will have a long term solid performance and economic value, that's really hard to do.” - After waiting five months between tests, the safe landing of RPX-08 leaves the flight line energized, setting high expectations for the next test with lighthearted optimism: “It'll be fine. It'll be just fine.”
---
[01:04:07](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3847s) The RPX-09 Breakup: Disproportionate Solutions in Flight Control
The mood shatters during flight test RPX-09. Over the comms, an engineer calls out in shock as the kite bounces violently onto the tether and disintegrates: “Oh sh* bouncing onto the tether, kite just broke into many pieces.” The crash immediately triggers safety protocols, including the emergency checklist titled *Makani M600 Electrical Safety After a Hard Landing*, while ground crews survey the debris field where the impact marks and tether rest.
```mermaid flowchart TD accTitle: RPX-09 Failure Analysis and Resolution accDescr: Root cause analysis diagram mapping kite breakup back to rudder ineffectiveness and software control fixes. A["RPX-09 Mid-Air Breakup"] --> B["Analyze Flight Telemetry Data"] B --> C["Identify Physical Deficit: Rudder Ineffective"] C --> D["Aero Redesign: Enlarge Rudder Surface"] B --> E["Controls Finding: Software Mismatch"] E --> F["Controls Fix: A Few Lines of Code"] D & F --> G["High-Confidence Fixes Prevent Recurrence"] ```
The post-crash investigation highlights the vital difference between pure computer simulations and physical testing: - Flight telemetry revealed that the aerodynamic rudder was significantly less effective in actual flight conditions than aerodynamic models had predicted. - Without real-world flight data, the team would have spent years operating inside flawed simulations without recognizing that control authority was deficient under specific dynamic states. - The control team notes a fundamental law of guidance and control engineering: “One thing I've learned in Controls is that the size of the solution is often unrelated to the size of the problem.” - While the failure resulted in the total destruction of the airframe, the engineering fixes were tight and manageable: enlarging the rudder surface area and modifying a few critical lines of control code to handle edge-case flight states.
---
[01:05:26](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3926s) Moving Beyond Containerhenge: Ground Station Testing
The RPX-09 crash serves as an operational checkpoint. For months, the team had relied on “Containerhenge”—a provisional test rig fashioned out of stacked shipping containers—while the permanent ground station was being designed and manufactured. With the new ground station hardware finally assembled, Makani splits its focus: one branch of the team diagnoses the mid-air breakup, while the flight operations team begins hover qualification testing on the new ground station before shipping the entire system to a high-wind site at Parker Ranch on Hawai’i.
```mermaid flowchart LR accTitle: Pre-Hawai'i Ground Station Validation accDescr: Sequence showing ground station tether hover tests leading into packaging for Parker Ranch deployment. subgraph Station["Ground Station Validation"] A["Retire 'Containerhenge' Rig"] --> B["Test New Automated Ground Station"] B --> C["Constrained Hover Off Ground Peg"] end subgraph Deployment["Deployment Gate"] C --> D["Risk Tradeoff on Legacy Airframe"] D --> E["Final Hardware Schedule Window"] E --> F["Ship Complete System to Hawai'i"] end ```
The pressure during this final testing window is intense: - Testing at Alameda is constrained by poor wind and tight project timelines: “This is the last week of testing, hopefully, before we go to Parker Ranch. There's no more tests on the schedule after that.” - The team executes delicate hover liftoffs directly from the ground station panel peg, backing out and returning toward the perch. - Operators confront a high-stakes trade-off: an error during ground station hover could destroy both the ground station mechanism and the sole operational legacy airframe, stalling flight tests until a risky new kite can be prepped. - Team members embrace the existential drive of the mission to push through anxiety: “We gotta, we gotta move here. We got to save the freakin world.” - The operational mindset balances caution with courage: “If there was no fear of failure, I don't think it would be worth doing so I probably wouldn't be doing it.”
---
[01:07:24](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4044s) Parker Ranch, Hawai’i: Blending Futuristic Flight with Cultural Stewardship
Makani ships the complete system to the Island of Hawaiʻi, establishing a flight facility on Parker Ranch grassland near an active gravel quarry. The site balances exceptional wind resources with low exposure to air traffic, populated settlements, and livestock. Before beginning flight operations, the team joins local community leaders in a traditional Hawaiian blessing ceremony to consecrate the site and honor the connection to the land.
The partnership reflects a shared alignment on clean energy: - Hawai’i’s ambitious renewable energy goals make the island an ideal living laboratory for utility-scale clean technology. - The team equips the system’s electrical ground infrastructure, retrofitting power inverters with high-capacity energy dump systems to ensure safety margins during sudden load rejections. - The crew approaches mainland technology testing with humility: “As a technology company coming from the mainland we knew that testing our kite in Hawai'i was an extreme privilege, and we felt a sense of responsibility to do it right and to do it safely and to respect the people and the place.” - Observers marvel at the visual contrast of an ultra-modern carbon-fiber energy kite and white robotic ground station operating amidst vast, rolling tropical pastureland. - The ultimate goal for the flight campaign is defined not by novelty, but by routine reliability: “Well, not a couple of loops. We want to do so many loops that it becomes really really boring.”
---
[01:10:25](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4225s) All-Modes Flight Off the Robotic Ground Station
The Parker Ranch deployment marks the critical moment of the entire program: flying the M600 kite across all flight regimes while mechanically tethered to the robotic ground station. When Makani had first demonstrated all modes on the earlier Wing 7 prototype, coordinating the autonomous airframe with ground mechanics had proved exceptionally difficult. Coupling the much larger M600 to the rotating ground station carries immense financial and operational stakes, requiring an intricate sequence where the ground station arm rotates 90 degrees while the tether swings through a constrained operational corridor.
```mermaid flowchart TD accTitle: M600 All-Modes Flight Sequence accDescr: Step-by-step telemetry states during the M600 crosswind and perch cycle off the ground station. A["Vertical Hover Ascent"] --> B["Tether Engaged in Levelwind"] B --> C["Tether Payout Under Tension"] C --> D["Acceleration Phase (Accel)"] D --> E["Transition-In (Trans-In)"] E --> F["Full Crosswind Normal Loops"] F --> G["Transition-Out (Trans-Out)"] G --> H["Hover Retrieval & Perch Landing"] ```
After six months without flight tests, mission operations commands the sequence over live flight loops: - **Ascent & Payout:** The kite enters vertical hover, the conductive tether engages the automated levelwind mechanism, and payout begins with steady tension on the line. - **Transition-In & Crosswind:** Telemetry confirms rapid acceleration; the kite completes “trans-in,” locked tightly inside its flight corridor, and initiates circular crosswind loops generating high power with automated detwist tracking active. - **Flight Scale:** Observers are stunned by the sheer physical scale of the M600 sweeping across the sky: “Makani so far has brought kite energy up at a scale that no one has done before. And it is something very impressive to see such a big kite flying so low from the ground.” - **Transition-Out & Recovery:** The kite navigates slight overspeed warnings, enters crosswind prep trans-out, stabilizes in hover with payouts matched, engages the gain ramps, and brings the airframe safely to the perch. - Completing the full flight cycle reaffirms the Moonshot vision: “Seeing the kite fly loops, it's like that's the antidote to any sort of malaise. Go watch that kite fly loops and you will believe that this whole thing will be possible.”
[01:14:58](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4498s) The Strategic Pivot: Racing Offshore to Deepwater Wind
Autonomous crosswind flight without human intervention had finally been accomplished, but celebration was tempered by a shifting commercial landscape. Over the decade Makani spent honing its kite technology, conventional onshore wind turbines had advanced rapidly in scale and efficiency, eliminating the kite’s economic cost advantage on land. The onshore market opportunity had diminished, leaving stranded offshore wind resources over deep water as the clearest remaining frontier. Rather than proceeding in a comfortable sequence, the team committed to an 18-month sprint to prove the system could operate offshore from a floating platform, betting the future of the company on marine deployment before they had even finished validating ground station flight dynamics in Hawai'i or ensuring flight controls could reliably prevent another mid-air breakup.
The decision to tackle deepwater offshore while still confronting existential mechanical and control problems was driven by speed and the pressing threat of climate change. A methodical, one-variable-at-a-time engineering approach would have taken years that the venture simply did not have. As one team member explained regarding the compressed timeline: “It's because we didn't have enough time to do it methodically one thing at a time.” Deploying a kite from a floating buoy had to be initiated immediately because of the lengthy design cycles required. Another engineer emphasized the global stakes: “Having a low cost variable renewable resource that can be deployed deep deepwater would be of tremendous advantage to help solve that problem.”
- While fixed-bottom offshore wind turbines require shallow water near the coast, deepwater wind represents an enormous untapped energy reserve with strong, consistent winds. - Conventional deepwater wind turbines depend on massive, prohibitively expensive floating substructures to keep towering steel masts upright. - Eliminating the heavy tower allows airborne wind kites to operate from comparatively small, lightweight floating spar buoys at significantly lower capital and installation costs.
```mermaid flowchart TD accTitle: Offshore Wind Technical Comparison accDescr: Diagram contrasting traditional floating offshore wind turbines with Makani's lightweight spar buoy kite system in deep water.
subgraph Conventional["Traditional Offshore Wind"] T1["Massive Heavy Turbine & Tower"] --> T2["Huge Floating Substructure"] T2 --> T3["High Capital & Mooring Costs"] end
subgraph Makani["Makani Airborne Wind"] K1["Lightweight Energy Kite"] --> K2["Compact Floating Spar Buoy"] K2 --> K3["Low Material Mass & Cheaper Mooring"] end ```
[01:17:30](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4650s) Destination Norway: Offshore Engineering in Haugesund and Stavanger
Kite deployment in deep water promised direct access to vast coastlines located right beside dense coastal populations, unlocking clean energy for hundreds of millions of people. Seeking an ideal environment for marine testing, Makani headed to the maritime hub around Stavanger and Haugesund, Norway. The team immediately felt at home with the local maritime culture, which brought centuries of offshore experience and comfort with unpredictable ocean conditions. Describing the region's relationship with daring marine ventures, a team member observed: “Like they're in the business of doing strange things in the ocean.”
The Norwegian operation was designed to adapt Makani’s existing onshore hardware as directly as possible, compressing ground equipment onto a floating barge and spar setup. Yet operating in the North Sea introduced severe operational constraints. On land, a faulty part or sensor could be swapped out in the shop; offshore, even reaching the base station spar in rough seas or foul weather was hazardous, and once the vessel cast off, any unaddressed failure threatened to halt the entire campaign. As the team ticked off the countdown on the shop whiteboard—between 26 and 33 days until flight—they completed dry-run checks on the kite, tested spinning motors, and prepared the communication links across the untested sea-surface cable.
[01:20:21](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4821s) Havdrage 1 and the Sleipnir Lift: Preparing for Tow-Out
The offshore floating spar was christened *Havdrage 1*, playing on a Norwegian double meaning: *drage* translates to both “kite” and “dragon.” With the tow-out date just two days away, the culmination of 18 months of design and fabrication came down to a high-stakes crane lift. Working alongside the heavy lift vessel *Sleipnir*, the crew hoisted the kite and mounted it onto its perch on the floating structure. Normally, deepwater offshore engineering programs require many years of iterative design; Makani had compressed the entire offshore spar integration into a breakneck year and a half.
Reflecting on the sheer audacity of the schedule, an engineer remarked: “A plan was laid out that looked, I would say, bordering on impossible.” Standing beside the newly mounted kite, team leaders offered heartfelt thanks to members like Crystal, Alan, and Luis, who were handing over the physical hardware they had built and tuned, trusting that every component would endure the harsh marine elements. The collective effort across multiple engineering disciplines turned a speculative vision into steel, composites, and carbon resting over the water. As one team member summarized the shared relief and unity: “All these teams working together have put together something that we individually might have thought, 'this is impossible'.”
[01:22:20](https://www.youtube.com/watch?v=qd_hEja6bzE&t=4940s) Going Independent with Shell: Connecting the Sea Surface Cable
The offshore campaign coincided with a pivotal organizational transition. Makani had spun out from Alphabet's X to become an independent commercial company, partnering with Shell to demonstrate kite viability in the offshore environment where its value proposition was greatest. Only six months after their first autonomous crosswind flight on a land ground station in Hawai'i, the crew was positioned on the other side of the world attempting to replicate the feat from an unanchored, moving buoy. A single seasonal testing window remained: after spending the spring flying in Hawai'i, the crew had only a few weeks of Norwegian summer before North Sea conditions would become too violent to fly.
The dynamics of landing on an ocean buoy introduced unprecedented control challenges that pure analytical equations could no longer address. The kite needed to land autonomously on a base station platform swaying, rolling, and heaving on ocean waves, requiring complex dynamic computer simulations. Past 8:00 p.m. on a quiet Sunday evening with mirror-flat seas, technicians made the mechanical and electrical connections for the sea-surface umbilical cable. The moment of truth arrived as the team powered up the system remotely to verify communications, pull the first dynamic measurements of buoy movement, and confirm GPS tracking, celebrating when telemetry responded cleanly without any blown circuits.
[01:24:35](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5075s) Flight Day in the North Sea: Morning Boat Commute and Game Time
Flight day began with a scenic 15-minute boat commute across Norwegian waters at sunrise—a stark aesthetic contrast to the dusty desert runs of China Lake or the grassy volcanic slopes of Parker Ranch. The weather forecast called for a steady, building breeze, creating favorable conditions for launch. The team tempered expectations by defining baseline milestones: simply launching off the floating perch and gathering real telemetry on how the kite tracked the rolling spar from a few meters away would validate the hydrodynamic simulations and yield invaluable engineering data.
While simulations predicted that vertical launch, tether reel-out, trans-in, and crosswind flight would proceed smoothly, returning to the moving perch remained the most perilous phase of the mission: “The biggest challenge in the test will be of course to land.” Nine time zones away in Alameda, California, dozens of Makani engineers gathered at the company's headquarters around midnight with pizza and breakfast to watch the live video feed. Out on the water, the flight operators settled into their stations, counted down to game time, dialed the throttle setting just beneath 0.8, and called out that all systems looked ready for flight.
- Commuting by marine vessel to an offshore spar buoy marked the culmination of a decade-long testing journey that previously spanned desert test sites and island ranches. - Launching from the floating spar provided the first real-world verification of Makani’s coupled aerodynamic and hydrodynamic computer simulations. - Crosswind flight and hover operations were fully monitored in real time across the Atlantic via secure telemetry feeds linking the North Sea barge to Makani headquarters in California.
[01:26:47](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5207s) Aborted Landing and Perch Realignment
During operations offshore, the flight crew monitors the kite's return to the floating perch. As gain ramps smoothly and the kite dips slightly before stabilizing, tension reads steady at 9 kN. Suddenly, the telemetry flags a problem: the levelwind elevation angle misreports at roughly 39 to 40 degrees, throwing off the automated recovery path. The operator cross-checks visual cues from the perch, confirming the kite remains aloft, and opts to descend manually while monitoring critical clearance milestones: payout steps drop steadily from 1.5 meters to 1 meter, the bridles clear, and the hooks clear at 50 centimeters.
```mermaid flowchart TD accTitle: Perch Recovery Sequence and Failure Mode accDescr: Steps showing the descent toward the perch hooks followed by the levelwind angle mismatch and sawtooth skip. subgraph Descent["Controlled Approach"] A["Elevation Angle Anomaly (39°-40°)"] --> B["Manual Payout Down to 50 cm"] B --> C["Bridles & Hooks Clear Perch"] end subgraph LatchAttempt["Perch Engagement"] C --> D["Starboard Hook Enters Tooth"] D --> E["Port Hook Approaches"] E --> F{"Tooth Engagement"} F -->|"Skips Sawteeth"| G["Emergency Gain Ramp Down / E-Stop Prep"] F -->|"Hold & Inspect"| H["Identify Fault & Recalibrate"] end ```
As the ground station sensors fluctuate near proximity thresholds, the starboard hook reaches the alignment teeth, but descending onto the perch causes the assembly to slip: “It just skipped a bunch of teeth, is it... did we gain ramp?” The operators confirm the gain ramp is down, consider an emergency stop on the ground station winch, verify that the starboard hook is holding in the sawtooth bracket, and pause the descent. The engineering crew quickly identifies the sensor fault, corrects the mechanical alignment, and prepares the platform for a fresh offshore launch.
[01:28:36](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5316s) Successful Offshore Launch into the North Sea
With the sensor recalibrated and engagement sensors reading properly at zero elevation angle, the winch brake is disengaged. Payout accelerates smoothly, the elevation angle stabilizes at nine degrees, and GPS tracking reconciles across ground station instruments. Passing 100 meters altitude and roughly 300 meters of tether payout, the ground station maintains clean azimuth tracking without gate alarms. Operators initiate the hover-acceleration sequence, pitching the kite forward into the flight playbook with throttle above 0.8:
```mermaid flowchart LR accTitle: Offshore Flight Transition Sequence accDescr: Stages of the offshore launch from winch payout to full crosswind flight. subgraph Payout["Winch & Ascend"] A["Zero Elevation / Brake Release"] --> B["Payout Past 300m / Alt 100m"] end subgraph Transition["Playbook Injection"] B --> C["Throttle > 0.8 & Pitch Forward"] C --> D["Return to Tethersphere"] end subgraph Crosswind["Power Generation"] D --> E["Aero Angles at 90°"] E --> F["Crosswind Loops in North Sea"] end ```
The kite transitions cleanly back into the tethersphere, the detwist mechanism tracks properly, and the craft initiates broad crosswind loops over the water with wind conditions steady at 9.7 m/s. Observing the buoy reacting to tether loads and the wing banking gracefully through three o'clock, the crew revels in achieving something unprecedented: “Can you guys believe that, we're flying crosswind in the North Sea?! So cool.”
Reflecting on the scene, team members note how mature technologies like standard horizontal-axis wind turbines appear natural only because decades of incremental refinement stripped away unnecessary complexity: - One team member cites Antoine de Saint-Exupéry’s design philosophy: “You know, a machine achieves perfection not when there's nothing left to add, but when there is nothing left to remove.” - Another engineer invokes the Chinese idiom *hèng kōng chū shì* (横空出世), describing an entity appearing out of nowhere: “It's like something you feel that it's never been there, but it just emerges suddenly. At first, you don't know what it would do. But once you see it, you know, take off and function you say, Ah! Like this is something that it's born to do.” - Flying high above the water shifts spatial perspective, making the open sea look deceptively compact when viewed from distant chase vessels.
[01:31:14](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5474s) Crosswind Trans-out and Loss of the M600
After an hour of stable crosswind figure-eights, changing weather conditions force the team to plan an egress. The flight crew spots rising swells that threaten the safety limits for offshore crew transfer vessels, and the southwest wind begins dying down. To stay ahead of the weather, flight operations schedules the transition out of crosswind (trans-out) for 1:30, initiating prep at the apogee of the subsequent loop.
The kite initiates crosswind prep trans-out from high in the window. As it drops towards hover, the tether dynamics alter drastically against the moving buoy base: - The floating buoy sits noticeably displaced under dynamic marine currents. - Roll angle begins diverging rapidly, climbing past 30 to 40 degrees. - Ground station operators scramble as control authority decays: tether pitch hits 100, hover pilot commands back-pitch to minus 70, elevation angle plummets toward six degrees, and throttle maxes out. - With instability escalating and the kite unable to arrest its descent, flight directors command: “E-stop everything.”
The kite hits the water, failing to recover to hover or return to the perch. While the loss of the airframe stings, leadership underscores the experimental imperative. Executive Charlie stresses that staying tethered to shore out of fear would be far more damaging: “The kite landed in the ocean, it did not come back and land on the perch, which on the surface of it, sure, OK, yes, that's a failure. But I can tell you, what would be an even bigger failure. It would be failure to launch.” The team will spend a year analyzing the telemetry data, noting that the crash resolved crucial unknowns about hover recovery dynamics at sea.
[01:34:19](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5659s) Aftermath, Octoberkite, and Hawaii Testing
Inspecting the wreckage at dock, technicians note how the airframe broke apart, pointing out that the mass balance tube remained attached solely by the internal wing harness wiring—composed of power-over-fiber lines and heavy copper conductors. The emotional toll of seeing months of hand-crafted composite work destroyed is palpable across the shop floor. When asked how it feels to build machines that end up crashing, one engineer replies: “You trying to make me cry right now? You know what, I was really ecstatic to see the kite fly. And I watched it for the whole hour that it flew crosswind. And that was amazing. Like, who can say that they were a part of achieving something so beautiful, you know? And heart wrenching at the same time.”
The flight analysis exposes a fundamental control limitation during hover:
| Flight Condition | Required State | Failure Mechanism Encountered | |:--- |:--- |:--- | | **Hover Stance** | Horizontal tether angle & sustained tension | High elevation angle & slack line near ground station | | **Buoy Coupling** | Predictable anchor coordinate | Marine displacement drifting beneath kite trajectory | | **Recovery Strategy** | Aerodynamic control authority | Insufficient yaw/roll authority once kite drifts overhead |
Parallel to the offshore operation, a rapid sprint called "Octoberkite" had been working on a re-winged airframe: - Designed as a 3-month project to conclude by October, intended for deployment by early 2021. - Kept the advanced internal avionics, actuators, and motor controllers while transferring them to a larger carbon-fiber wing structure to boost wing area, lift, and power generation. - Back in California, engineers loaded flight data into the simulator, revised controller algorithms, and transitioned operations to the Parker Ranch test site in Hawaiʻi for the fall and winter to test control fixes before returning to Norway.
[01:38:41](https://www.youtube.com/watch?v=qd_hEja6bzE&t=5921s) Financial Headwinds and the Legacy of Radical Innovation
Flight operations in Hawaiʻi proceed in smooth trade-wind conditions, testing new ascend modes, gain ramps, and improved tether engagement loops. Yet outside the test field, Makani faces a severe existential roadblock. Having spun out of Alphabet's moonshot factory (X), the venture is tasked with securing external capital to fund development: - Offshore operations in deep water proved kites could fly from floating spar buoys where conventional fixed-bottom turbines cannot go. - Designing, manufacturing, and deploying the scaled Octoberkite alongside recurring North Sea test charters requires massive capital reserves. - Commercial viability demands years of continuous runtime to prove multi-thousand-hour mean time between failures (MTBF). - After thirteen years of uninterrupted engineering, the team is unable to find the private investment needed to finance the long runway toward commercial deployment: “After 13 years of setting goals, meeting them and setting new goals, the end of our path was suddenly glaringly in front of us.”
Reflecting on the historical arc of renewable power, team members recall the 1940s Smith-Putnam wind turbine—an engineering triumph that proved electricity could be generated at utility scale, only to be shut down and mothballed for 30 years because coal was 50 percent cheaper at the time. Makani's engineers maintain that airborne wind systems represent the ultimate structural endgame for wind capture by eliminating hundreds of tons of steel and concrete tower mass: “It is significantly less mass. And you don't have all this extra stuff to just harness the power.” Despite the commercial halt, the team takes pride in proving the physics of deep-water airborne generation, arguing that civilization requires audacious leaps for future generations even when initial economics outpace the market.
[01:41:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=6102s) The Audacity to Tackle the Hardest Problems
Reflecting on the deeper purpose behind the project, team members articulate why undertaking such high-risk technical challenges matters far beyond the engineering itself. There is a generational responsibility: society needs audacious pursuits so younger generations have figures of real technical courage to inspire them. As one team member explains, “You have to be audacious so that children have astronauts to look up to and heroic engineers and they get to see people working on things that are hard and see the struggle.” More urgently, the imperative is ecological and existential: “But I also think we have to do it for our children because we owe them a planet that works and the timelines are getting shorter and the level of effort is not getting any less.”
The outside perception of Makani often assumed an operation backed by massive corporate headcount, but the reality was far more concentrated and intimate. A team member notes that people frequently assumed Makani employed hundreds of staff given the scale and visibility of the hardware, observing, “And if you really look to it we're only a few tens of people doing all the good work that led to those crazy experiments.” At its heart, the core activity maintained a sense of wonder—flying a kite to advance renewable energy and leave behind a kinder world. When asked whether the team ever achieved the aerospace engineering holy grail of making flight testing routine and boring, the response is bittersweet: “I think not. Sadly, but also like very joyfully not. It was never boring.”
The closing narration sums up the thirteen-year odyssey of Makani. Over more than a decade of attempting to pull utility-scale energy from high-altitude winds, lives unfolded in parallel with the technology: teammates grew older, babies were born, and the broader energy landscape shifted while the team stayed laser-focused on their singular mission. While the project did not reach commercial deployment, the journey redefined the boundaries of what is technically achievable. When confronting climate change, waiting for safe, incremental, or guaranteed solutions is insufficient. As the narrator concludes: “We have to risk the chance that we will fail because that is the only way we can possibly succeed.”
- **Scale of the core team:** Only a few dozen people designed, built, and operated the full-scale energy kite systems and offshore testing campaigns. - **Duration:** 13 years spent developing airborne wind energy technology from early small-scale prototypes to utility-scale tethered flight. - **Philosophy of moonshots:** Pushing past conventional thinking requires plunging into problems that seem impossible and accepting the inherent risk of public failure.
---
[01:49:36](https://www.youtube.com/watch?v=qd_hEja6bzE&t=6576s) Post-Credits: Sweeping the Desert
In a brief, tongue-in-cheek post-credits scene, a team member is filmed methodically sweeping the vast, dusty ground at the desert flight test site with a push broom. Looking out over the arid expanse and broom in hand, they wryly summarize the absurdity of the chore: “Sweeping the desert. An endless but noble task.”
Pondering what this ritual signifies in the grand lineage of the project, they muse out loud to the camera crew about dedicating the moment to subsequent generations of hardware: “For the future energy kites... I don't think this is really a poem... so much as the beginning of a novel. Or maybe a dramatic speech.” The deadpan moment captures the self-deprecating humor and unglamorous grit that underpinned daily life at the Makani test sites.
## Notable quotes > [01:04:07](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3847s) One thing I've learned in Controls is that the size of the solution is often unrelated to the size of the problem.
> [01:41:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=6102s) You have to be audacious so that children have astronauts to look up to and heroic engineers and they get to see people working on things that are hard and see the struggle.
> [22:12](https://www.youtube.com/watch?v=qd_hEja6bzE&t=1332s) Working on something hard for a long time as part of a team and watching it work exactly as you'd intended it to is as good as it gets.
> [01:41:42](https://www.youtube.com/watch?v=qd_hEja6bzE&t=6102s) We have to risk the chance that we will fail because that is the only way we can possibly succeed.
> [01:05:26](https://www.youtube.com/watch?v=qd_hEja6bzE&t=3926s) If there was no fear of failure, I don't think it would be worth doing so I probably wouldn't be doing it.
## Mentioned Makani, Miles Loyd, Santa Cruz, Wing 6, Munho, Tommaso Romanelli, Anita, Wing 7, Google.org, U.S. Department of Energy, ARPA-E, Corwin Hardham, Google X, Alphabet, Containerhenge, Rocket Jeff, Nicholas, SN1, SN2, Birdcage, China Lake, M600, Johnny, RPX-08, RPX-09, Alameda, Parker Ranch, Hawai’i, Haugesund, Stavanger, Norway, North Sea, Havdrage 1, Sleipnir, Shell, Octoberkite, Crystal, Alan, Luis, Charlie, Antoine de Saint-Exupéry, Smith-Putnam wind turbine
## Video description "Pulling Power From the Sky: The Story of Makani" chronicles the thirteen-year quest of an eclectic band of scientists, artists, sailors, pilots, and engineers as they team up to design and build kites that can efficiently harness energy from the wind. Created by members of the Makani team, and featuring beautiful footage from test sites in Hawai’i, California, and Norway, this film provides an intimate portrait of the team and spirit.
For more information about Makani, please see The Energy Kite, available at x.company/projects/makani
[Source](https://www.youtube.com/watch?v=qd_hEja6bzE)