Joe Scott
Deploying an orbital sunshade constellation to halt global warming would bankrupt the world economy and emit billions of tons of carbon dioxide, making direct terrestrial clean energy investment far more practical.
AI-assisted summary of Space Shades: Humanity's Last Hope | Answers With Joe — original source. Check the original for full context.
Source published:
Key ideas
- Blocking just 2% of incoming sunlight at Lagrange Point 1 (L1) would offset accumulated global warming, requiring an occluding surface area of roughly 2.6 million square kilometers—equivalent to about one-third of the continental United States. (5:01)
- Deploying such a shield from Earth using SpaceX Starship within a 10-year window would demand nearly 2.9 million launches—roughly 719 launches every single day—costing trillions in launch operations alone. (9:41)
- Manufacturing the estimated 43.5 billion steerable shades would cost upwards of $2.175 quadrillion to $4.35 quadrillion, far surpassing total global gross domestic product of approximately $81 trillion. (11:18)
- The 2.9 million Starship launches would inject roughly 7.7 billion metric tons of CO2 directly into Earth's atmosphere, substantially undermining the environmental benefits of the shade. (16:59)
- A more technically feasible alternative involves autonomous lunar manufacturing and electromagnetic railguns, though researcher Roger Angel notes the same capital applied directly to terrestrial renewable energy would deliver far better and permanent results. (20:39)
Detailed notes
## Background Published on YouTube on August 3, 2020, by science communicator Joe Scott on his channel Answers With Joe, this video investigates the concept of placing a massive solar shade in space as a last-resort geoengineering solution to runaway climate change. Grounded in research by astronomer Roger Angel and astrophysicist Ethan Siegel, the presentation examines the scale, cost, launch logistics, and physical feasibility of blocking solar radiation to cool the planet.
## TL;DR Joe Scott conducts a detailed engineering and economic thought experiment to determine whether deploying a sunshade at Lagrange Point 1 (L1) could realistically reverse global warming by blocking 2% of solar irradiance. Calculating the required 2.6 million square kilometer coverage area, he demonstrates that deploying the array using SpaceX's Starship would demand nearly 2.9 million launches, cost trillions or quadrillions of dollars, and emit billions of tons of carbon dioxide during launch alone. After examining speculative workarounds such as autonomous lunar manufacturing and electromagnetic railguns, Scott concludes that treating space shades as an emergency escape hatch is an impossible distraction, echoing Roger Angel's verdict that the same capital and innovation should be applied directly to terrestrial clean energy.
## Atmosphere & style The presentation blends conversational, geeky enthusiasm with sharp, deadpan wit, pulling viewers along a thought experiment that rapidly escalates from plausible sci-fi optimism into mathematical absurdity. Scott balances accessible visual comparisons—like stacking trillions of dollar bills past the Sun to Mars—with rigorous orbital mechanics, delivering sobering realities with a lighthearted, self-deprecating touch. The narrative arc moves from curious exploration to incredulity at the sheer logistical impossibility, ultimately landing on a grounded, pragmatic plea for investing in real-world environmental action.
## Bulletin - [05:01](https://www.youtube.com/watch?v=6yqi0FabHHs&t=301s) Blocking just 2% of incoming sunlight at Lagrange Point 1 (L1) would offset accumulated global warming, requiring an occluding surface area of roughly 2.6 million square kilometers—equivalent to about one-third of the continental United States. - [09:41](https://www.youtube.com/watch?v=6yqi0FabHHs&t=581s) Deploying such a shield from Earth using SpaceX Starship within a 10-year window would demand nearly 2.9 million launches—roughly 719 launches every single day—costing trillions in launch operations alone. - [11:18](https://www.youtube.com/watch?v=6yqi0FabHHs&t=678s) Manufacturing the estimated 43.5 billion steerable shades would cost upwards of $2.175 quadrillion to $4.35 quadrillion, far surpassing total global gross domestic product of approximately $81 trillion. - [16:59](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1019s) The 2.9 million Starship launches would inject roughly 7.7 billion metric tons of CO2 directly into Earth's atmosphere, substantially undermining the environmental benefits of the shade. - [20:39](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1239s) A more technically feasible alternative involves autonomous lunar manufacturing and electromagnetic railguns, though researcher Roger Angel notes the same capital applied directly to terrestrial renewable energy would deliver far better and permanent results.
## Key takeaways - [01:21](https://www.youtube.com/watch?v=6yqi0FabHHs&t=81s) Planetary surface temperature is determined by incoming solar radiation and atmospheric heat retention; altering solar input becomes an option if emissions cuts cannot prevent tipping points. - [01:21](https://www.youtube.com/watch?v=6yqi0FabHHs&t=81s) Terrestrial geoengineering techniques like stratospheric aerosol injection mimic volcanic events but carry unpredictable, virtually irreversible ecological risks. - [03:51](https://www.youtube.com/watch?v=6yqi0FabHHs&t=231s) Lagrange Point 1 (L1), situated 1.5 million kilometers sunward from Earth, is the ideal orbital station because solar and terrestrial gravitational forces balance out. - [05:01](https://www.youtube.com/watch?v=6yqi0FabHHs&t=301s) Geometric calculations show that a 2% reduction in solar irradiance requires a sunshade spanning 2.6 million square kilometers at L1. - [07:16](https://www.youtube.com/watch?v=6yqi0FabHHs&t=436s) A modular swarm of mid-sized, steerable shades is superior to a single monolith or uncontrolled dust clouds, offering structural redundancy and controllable solar deflection. - [09:41](https://www.youtube.com/watch?v=6yqi0FabHHs&t=581s) Maximized cargo packing inside SpaceX Starship limits payload to flat discs, requiring 15,000 stacked shades per launch to cover 0.9 square kilometers per flight. - [09:41](https://www.youtube.com/watch?v=6yqi0FabHHs&t=581s) Achieving the 2.6 million km² target in 10 years would require 719 Starship launches daily, a cadence physically impossible with current or near-future infrastructure. - [11:18](https://www.youtube.com/watch?v=6yqi0FabHHs&t=678s) Constellation manufacturing costs range between $2.175 quadrillion and $4.35 quadrillion, which is tens of times larger than total annual global GDP. - [13:40](https://www.youtube.com/watch?v=6yqi0FabHHs&t=820s) Purely opaque shades would act as uncontrollable solar sails; materials must scatter light (such as Fresnel lenses or diffusive glass) or reradiate thermal heat to remain on station. - [16:59](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1019s) Station-keeping thrusters would face severe fuel scarcity, as global xenon production is just 6 tons annually and argon supplies are heavily committed to other industries. - [16:59](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1019s) Rocket exhaust from nearly 2.9 million Starship flights would release 7.7 billion tons of CO2, creating an emissions burden comparable to global commercial aviation. - [20:39](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1239s) Relocating production to the Moon leverages low gravity, abundant regolith, and lack of atmospheric friction, enabling lunar railguns to launch pre-assembled shade pods toward L1. - [22:19](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1339s) Sunshades act strictly as a temperature band-aid and fail to resolve secondary greenhouse gas impacts, including ocean acidification. - [24:17](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1457s) Even sunshade pioneer Roger Angel concluded that applying the massive capital and technological effort directly to terrestrial clean energy provides a vastly superior, permanent solution.
## Detailed walkthrough ### [00:00](https://www.youtube.com/watch?v=6yqi0FabHHs&t=0s) Climate Urgency and Drastic Solutions
While the energy transition is showing signs of progress—renewable power is expanding rapidly, cleaner technologies are transforming the electric grid, and major automotive manufacturers are finally taking electric vehicles seriously—it remains insufficient. Global population growth and expanding industrialization in developing countries mean carbon dioxide emissions continue to break records annually. Faced with increasingly dire projections from climate scientists, humanity risks crossing an irreversible tipping point where conventional decarbonization cannot act fast enough.
```mermaid flowchart TD accTitle: Planetary Energy Balance accDescr: The two core drivers determining planetary surface temperatures. subgraph Drivers["Planetary Heat Mechanics"] A["Incoming Solar Radiation"] --> C["Planetary Temperature"] B["Atmospheric Trapping (Greenhouse Effect)"] --> C end ```
In the search for drastic interventions, an idea frequently brought up is placing a massive solar shade in space to intercept sunlight before it reaches Earth, bringing average global temperatures back to pre-industrial baselines. As Joe Scott introduces his deep dive into the engineering and logistical reality of this proposal:
> “Assuming things continue at this pace we may reach a point of no return, a point where it's going to take something really drastic to turn things around.”
[01:21](https://www.youtube.com/watch?v=6yqi0FabHHs&t=81s) Terrestrial Geoengineering and Its Risks
At a fundamental level, planetary temperature is dictated by just two factors: the volume of solar radiation entering the system and how much of that heat the atmosphere traps. While cutting emissions to restore atmospheric equilibrium is the safest route, modifying incoming solar radiation becomes an attractive alternative if emissions cuts fall short. Earth-based geoengineering concepts attempt this within the atmosphere:
- **Cloud Seeding:** Injecting particles into the upper atmosphere to create high-albedo, reflective cloud decks. The downside is their ephemeral lifespan, which would demand thousands of continuous jet flights emitting vast quantities of greenhouse gases, largely defeating the initial purpose. - **Stratospheric Aerosols:** Injecting reflective dust or sulfur dioxide directly into the stratosphere, modeled after historical volcanic eruptions. - **Volcanic Analogues:** On June 15, 1991, Mount Pinatubo in the Philippines blasted 15 million tons of sulfur dioxide into the stratosphere, dispersing a global haze that reduced global average temperatures by 1°C over the following year. A similar phenomenon occurred with the 1815 eruption of Mount Tambora, resulting in the notorious "Year Without a Summer." Mount Pinatubo, however, was the first event observed in real time by orbital satellites.
Despite being technically plausible using high-altitude balloons, deploying 15 million tons of aerosols into the stratosphere carries immense risks. The ecological side effects cannot be predicted in advance, and atmospheric geoengineering is exceedingly difficult to reverse once initiated. Scott cautions against recklessly altering our atmosphere, noting that “it wasn't the machines that blacked out the sky in The Matrix.”
[03:51](https://www.youtube.com/watch?v=6yqi0FabHHs&t=231s) Placing the Shade at Lagrange Point 1 (L1)
If humanity set a 10-year deadline to construct an extraterrestrial shade to bypass atmospheric risks, the very first step would be determining where to station it. The location dictates the dimensions the shade requires. Stationing an object between the Sun and Earth points directly to Lagrange Point 1 (L1).
Lagrange points represent orbital gravitational balance areas where the competing pulls of the Earth and the Sun, along with orbital mechanics, keep an object in a fixed position relative to Earth:
- **Lagrange Point 1 (L1):** Located roughly 1.5 million kilometers sunward between Earth and the Sun, directly inline with solar radiation. - **Lagrange Point 2 (L2):** Located on the opposite side of Earth, away from the Sun, serving as the future station for deep-space observatories like the James Webb Space Telescope.
```mermaid flowchart LR accTitle: Orbital Alignment of L1 and L2 accDescr: Spatial order from the Sun through Earth to the James Webb Space Telescope position. Sun["Sun"] --> L1["L1 (1.5M km from Earth)"] L1 --> Earth["Earth"] Earth --> L2["L2 (JWST Location)"] ```
Scott explains the orbital mechanics to newcomers:
> “L1 stands for Lagrange Point 1, and Lagrange points are areas around the Earth or any orbiting body for that matter where the gravity of the Earth and the gravity of the Sun kind of even each other out.”
[05:01](https://www.youtube.com/watch?v=6yqi0FabHHs&t=301s) Calculating the Shade Area: 2.6 Million Square Kilometers
According to feasibility models—specifically astrophysicist Ethan Siegel’s analyses on *Starts With A Bang* and an exhaustive 2006 study published in the *Proceedings of the National Academy of Sciences* (PNAS) by Professor Roger Angel—humanity does not need to block the entire Sun. Shading just 2% of the incoming solar radiation would be sufficient to counteract accumulated warming and restore pre-industrial climate conditions.
Calculating that 2% requires first determining the footprint of a 100% occlusion disk at L1: - Earth's physical diameter is 12,742 kilometers. - Because the Sun is much larger than Earth, incoming sunlight forms a tapered cone. L1 sits 1.5 million kilometers upstream along that cone, approximately 1% of the total 149.6-million-kilometer distance between Earth and the Sun. - Factoring in this geometry, the required coverage diameter at L1 expands by roughly 1% to **12,869 kilometers**. - Applying the area of a circle ($\pi r^2$) produces a 100% cross-sectional area of **129,984,558 square kilometers**. - A 2% reduction requires blocking **2,599,691 square kilometers**, rounded off to **2.6 million square kilometers**.
To contextualize that size for the viewer:
> “Well it comes out to almost exactly the combined areas of the states of Washington, Oregon, California, Nevada, Utah, Idaho, Arizona, Montana, and Wyoming. About a third of the continental United States.”
Covering a footprint that massive qualifies as a colossal megaproject.
[07:16](https://www.youtube.com/watch?v=6yqi0FabHHs&t=436s) Monolith vs. Swarm Architecture
Building an umbrella measuring 2.6 million square kilometers cannot happen in a single launch; it necessitates an architectural framework that can be assembled or coordinated in deep space. Three distinct configurations present themselves:
1. **A Single Monolithic Shade:** - *Advantages:* Offers simplified command and control over a single consolidated vehicle. This simplicity matters because L1 is technically meta-stable ("stable-ish") and demands continuous station-keeping maneuvers against solar radiation pressure and orbital perturbations. - *Disadvantages:* Lacks redundancy. A strike by an errant piece of space debris could tear or spin the entire structure out of alignment. Furthermore, assembling millions of square kilometers requires endless dockings, each presenting an opportunity for critical failure.
2. **A Free-Flying Swarm of Independent Shades:** - *Advantages:* Provides modularity and structural redundancy. If individual units degrade or fail, the larger array continues functioning. - *Disadvantages:* Introduces a heightened probability of collisions among neighboring units should guidance and attitude thrusters fail.
3. **A Cloud of Micro-Shades:** - Breaking the concept down into microscopic or lightweight components distributed en masse across the L1 region.
[08:14](https://www.youtube.com/watch?v=6yqi0FabHHs&t=494s) The Mid-Size Steerable Shade and the Starship Constraint
Evaluating the various concepts for solar radiation management, dumping an uncontrolled cloud of micro-shades, dust, or reflective debris into space to create an artificial haze suffers from the exact same fatal flaw as atmospheric geoengineering: it is essentially permanent, leaving humanity completely helpless if catastrophic unintended consequences arise. Because of this, Joe Scott favors mid-sized shades equipped with autonomous guidance units as the ideal compromise. With steerable shades, correcting an over-cooling mistake is as simple as rotating them sideways to let more sunlight through.
When considering shade geometry, engineers might be tempted to build enormous structures that rely on elaborate origami-like folding mechanisms that unfurl once deployed—much like modern satellite solar panels. However, Joe dismisses mechanical origami because moving parts introduce immense mechanical complexity, higher weight, and dozens of potential failure points. The real objective is to maximize the surface area delivered to the Sun-Earth Lagrange point 1 (L1) per launch using flat, simple, inexpensive discs that fit snugly inside a standard rocket fairing. To achieve maximum throughput, the mission demands the largest payload fairing available, which points squarely to SpaceX’s Starship:
```mermaid flowchart TD accTitle: Launch Fairing Diameter Comparison accDescr: A comparison of payload fairing widths across major rockets evaluated for sunshade deployment.
subgraph Fairings ["Rocket Fairing Diameters"] A["Saturn V / New Glenn<br>6.6 meters"] B["SLS Block 2 Cargo<br>8.4 – 10.0 meters"] C["SpaceX Starship<br>9.0 meters wide x 18.0 meters tall"] end
A -.->|"Insufficient volume"| D["Space Shade Deployment"] B -.->|"Expendable / Prohibitively costly"| D C ==>|"Fully reusable & maximum volume"| D ```
While NASA’s Saturn V carried a 6.6-meter payload fairing (comparable to Blue Origin’s New Glenn) and the proposed Space Launch System (SLS) Block 2 cargo vehicle could range between 8.4 and 10 meters, Starship remains the only viable contender. Starship offers a payload bay 9 meters wide by 18 meters tall, but its defining advantage is full reusability. As Joe Scott argues:
> “I'd argue that the Starship is really the only way to do this; you would have to have a fully reusable vehicle, and Starship's the only vehicle literally ever built that could do that.”
---
[09:41](https://www.youtube.com/watch?v=6yqi0FabHHs&t=581s) The Launch Math: From Fairing Limits to Absurdity
To see what launching a planetary sunshade looks like in practice, Joe Scott constructs an aggressively optimistic thought experiment. Assuming each circular shade can be engineered down to a razor-thin 1 millimeter thickness with an 8.75-meter diameter—leaving just enough edge clearance inside Starship’s 9-meter fairing for guidance modules—a single shade would dwarf an average person and cover roughly 60 square meters of surface area.
Because Starship cannot reasonably travel the entire 1.5-million-kilometer distance out to L1 and back, roughly 3 vertical meters of fairing height must be reserved for an onboard propulsion kick stage. This leaves 15 meters of usable vertical cargo height:
- **Shade dimensions**: 8.75 m diameter, 1 mm thick (~60 m² area per unit) - **Stacking capacity**: 15,000 shades packed into 15 vertical meters of fairing space - **Coverage per Starship launch**: 900,000 m² (0.9 km²) - **Total coverage target**: 2.6 million km² (to achieve a 2% reduction in solar irradiance) - **Total launches needed**: 2,888,888 launches
The launch cadence required to hit that target quickly spirals into sheer impossibility: - At a cadence of **one Starship launch every single day**, deploying the constellation would take **7,914 years**. - To complete deployment within an urgent **10-year window**, humanity would need to sustain **719 launches every single day**—amounting to one Starship lifting off every two minutes, 24 hours a day, for an entire decade.
---
[11:18](https://www.youtube.com/watch?v=6yqi0FabHHs&t=678s) Trillions and Quadrillions: Tallying the Impossible Bill
Even if the logistical bottleneck of launching every two minutes could be overlooked, the financial figures alone break the model entirely. Grounding launch cost estimates on Elon Musk’s November 2019 remarks to Air Force Lieutenant General John Thompson—where Musk projected an ultimate operating cost of $2 million per Starship flight—2,888,888 launches would cost $5.8 trillion purely in launch operations, without accounting for upper-stage propulsion or ground operations.
The manufacturing costs for the hardware are vastly more punitive. SpaceX manufactures Starlink satellites at roughly $250,000 per unit. While a passive shade disc seems simpler than an active communications satellite, operating autonomously 1.5 million kilometers away requires dedicated inter-satellite networking, thrusters, and autonomous station-keeping systems that can never be serviced:
- **Unit cost assumption**: $100,000 per shade disc - **Constellation size**: 43.5 billion individual shades (15,000 shades across ~2.9 million launches) - **Base manufacturing price tag**: $4.35 quadrillion
Even when cutting that unit estimate in half to $50,000 to generously factor in unprecedented economies of scale, the bill still totals $2.175 quadrillion. To illustrate just how incomprehensible that number is, Joe notes that stacking $2.175 quadrillion in physical one-dollar bills (at a standard thickness of roughly five bills per millimeter) creates a stack stretching 435 million kilometers:
> “That's far enough to reach the Sun, and then keep going and hit the Earth's orbit on the other side of the Sun, and then hit Mars.”
That physical stack of currency would cross the distance between Earth and the L1 Lagrange point 290 times over. Compared to the total global gross domestic product of approximately $81 trillion, manufacturing the shade array alone would cost nearly 26 times the annual economic output of planet Earth. As Joe summarizes: “Okay, so there's literally not enough money in the world to do this.”
---
[13:40](https://www.youtube.com/watch?v=6yqi0FabHHs&t=820s) Materials, Solar Wind, and the Fresnel Alternative
Beyond the absence of monetary capital, planet Earth faces severe material constraints. Shading 2.6 million square kilometers requires fabricating an artificial structure equal to the land area of two Colombias—or the entirety of Kazakhstan. The material selected must be super-abundant, dirt cheap, remarkably strong to survive rocket vibrations at a 1-millimeter thickness, and counterintuitively, somewhat transparent.
Drawing on the research paper by astronomer Roger Angel, Joe explains that a fully opaque sunshade placed in deep space would absorb the brute force of solar photons and the solar wind, acting as an unmanageable solar sail that gets pushed out of alignment. To stay in station, the disc must disperse or deflect photons rather than absorb their momentum:
- **Porous Sails**: Ultra-thin membranes perforated with micro-pores that let controlled amounts of radiation leak through. - **Micro-Slats**: Louvered venetian-blind style slats that deflect incident sunlight away at oblique angles. - **Diffusive Glass**: Highly specialized, ultra-thin silicate glass sheets (similar to advanced Gorilla Glass) that scatter light rather than block it. - **Fresnel Lenses**: Refractive sheets positioned to gently bend solar rays outward around Earth's orbital path. This method requires significantly greater surface area than pure shades to achieve the same cooling effect. - **Radiative Back-Surfaces**: Materials engineered to absorb photon energy on the sun-facing side and reradiate it out the back as thermal infrared heat to cancel out solar radiation pressure.
Procuring raw materials at this planetary scale would almost certainly require deep-sea floor strip-mining to avoid destroying vast swaths of populated farmland and continents.
---
[15:24](https://www.youtube.com/watch?v=6yqi0FabHHs&t=924s) The Industrial Scale and the Last-Ditch Paradox
The manufacturing infrastructure required to feed a 10-year deployment schedule would fundamentally reshape global geography. At 719 (or roughly 791) launches per day carrying 15,000 shades apiece, manufacturing plants would have to fabricate an astonishing 11,866,000 shades every single day.
Transporting nearly 12 million fragile, 8.75-meter wide glass discs daily across public highway or rail networks is physically impossible. The only logistical solution would be constructing hundreds of massive, dedicated manufacturing and launch megacomplexes directly adjacent to ocean coastlines worldwide, stamping out discs and immediately loading them into waiting Starship fairings.
This exposure of the industrial reality shatters the fantasy that space shades can serve as an emergency fallback plan:
> “The reason I've been using this arbitrary 10-year, you know, timeline here is because every single time people talk about this idea, it's sort of like a last-ditch effort; it's the thing that you do when everything else has failed and our entire existence hangs in the balance.”
If such a mega-engineering endeavor were ever actually undertaken, it could only realistically succeed as a multi-generational megaproject spanning at least a century. Yet framing space shades as a "last-ditch rescue plan" assumes humanity is already facing immediate climate catastrophe—a scenario where civilization has years, not centuries, to act.
[16:59](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1019s) Resource Scarcity, Thruster Fuels, and Rocket Emissions
Beyond the pure financial expense, the material extraction alone would be destructive to the planet, and the energy required to manufacture the shades is staggering. Worse still, there might not even be enough propellant to keep them stable once deployed at Lagrange point 1 (L1). The sunshades require control thrusters for station-keeping, which points toward ultra-efficient systems like miniaturized ion drives. However, these systems rely on noble gases such as xenon or argon. Xenon is essentially a non-starter because global production is only about six metric tons per year. While humanity produces roughly 700,000 metric tons of argon annually, it is already heavily utilized across other industries, leaving its viability as a dedicated shade propellant an unresolved question mark.
Another critical issue is decommissioning. Roger Angel estimated each shade would have an operational lifespan of roughly 20 to 30 years. Once they fail, they cannot simply be left behind, or collisions will trigger a catastrophic runaway debris cascade—an L1 version of the Kessler syndrome. Finally, the carbon footprint of the launches themselves presents an ironic obstacle. Citing calculations by Tim Dodd (The Everyday Astronaut), Joe notes that a single SpaceX Starship launch would generate approximately 2,683 tons of $\text{CO}_2$. Multiplying that by the required 2.9 million Starship launches yields an astonishing 7.7 billion metric tons of $\text{CO}_2$ pumped directly into the atmosphere, leading Joe to observe:
> “Multiply that by 2.9 million and we're putting 7.7 billion metric tons of $\text{CO}_2$ into the atmosphere, which seems to kind of defeat the point.”
For perspective, that emission volume is comparable on an annual basis to the global commercial airline industry, which accounts for roughly 2.5% of total worldwide greenhouse gas emissions.
- **Global noble gas production:** ~6 metric tons/year for xenon; ~700,000 metric tons/year for argon. - **Estimated operational lifespan:** 20 to 30 years per shade before disposal is required. - **Starship emissions per launch:** 2,683 tons of $\text{CO}_2$. - **Cumulative launch emissions:** 7.7 billion metric tons across 2.9 million launches.
---
[19:05](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1145s) Sci-Fi Workarounds: Railguns and the EmDrive
While Joe’s baseline calculations relied on technologies expected within the next five to ten years, Roger Angel’s proposal explored more radical, theoretical alternatives. Rather than relying entirely on chemical rockets, Angel proposed an electromagnetic railgun embedded into the side of a tall mountain or extending several miles upward to pierce the thickest layers of atmospheric resistance. Launching payloads every five minutes, this three-mile-high accelerator could impart the bulk of the escape velocity, requiring only minimal onboard propellant to nudge the payloads the rest of the way to L1.
On the shade side, another speculative concept involves replacing ion thrusters with propellantless propulsion, such as the controversial EmDrive. While experiments conducted by NASA’s Eagleworks showed anomalous thrust that was nearly indistinguishable from background air currents, an operational propellantless drive powered by onboard photovoltaic panels could theoretically keep shades stabilized indefinitely without consuming mass.
```mermaid flowchart TD accTitle: Earth vs Moon Space Shade Deployment Concepts accDescr: Comparison showing the Earth-based launch concept versus the lunar manufacturing and railgun deployment route.
subgraph EarthLaunch["Earth-Based Concept (Roger Angel)"] A["3-Mile-High Railgun / Starship"] --> B["Atmospheric Drag & High Fuel Burn"] B --> C["Onboard Ion Thrusters / EmDrive"] C --> D["Station-Keeping at L1"] end
subgraph MoonLaunch["Lunar Manufacturing Architecture"] E["Autonomous Lunar Factories"] --> F["Melt Regolith into Shades"] F --> G["Stack onto Pods (3 Weeks/Mo.)"] G --> H["Lunar Railgun Slingshot at L1 Approach"] H --> I["Deploy Shades & Reusable Pods Return"] end ```
---
[20:39](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1239s) The Ultimate Hack: Autonomous Lunar Manufacturing
The most viable long-term architecture circumvents Earth entirely by relocating automated production to the Moon. Operating under lunar gravity (one-sixth of Earth's) drastically reduces the energy required for construction and launch. Furthermore, the Moon is already roughly a quarter of the way to L1, lacks an atmosphere to impose fairing constraints, and provides an orbital slingshot velocity that can be exploited during specific launch windows.
Joe outlines a hypothetical automated system where robotic factories on the far side of the Moon harvest lunar regolith, refine it into shade structures, and extract aluminum to construct control modules. Earth would only need to ship sophisticated components that cannot be manufactured locally, eliminating the need for 800 launches a day from Earth's surface. Over three weeks each month, the factories would assemble and stack shades into transport pods. During the fourth week—when the Moon's orbit brings it closest to aligning with L1—electromagnetic railguns would fire the pods into space without burning propellant. After releasing their cargo at L1, the pods would fire thrusters to fly back to the lunar base, land, refuel, and repeat the cycle in a continuous, 24/7 autonomous loop.
- **Gravity advantage:** Lunar gravity ($1/6\text{g}$) requires drastically less fuel to achieve escape velocity. - **Operational schedule:** 3 weeks of continuous factory manufacturing and pod assembly followed by 1 week of railgun launches timed with the Moon's orbital alignment toward L1. - **Logistical profile:** Fully reusable transport pods deploy shades at L1 and return to the Moon to reload.
---
[22:19](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1339s) Economic Justification and the Opportunity Cost
Implementing such an infrastructure would demand unprecedented capital, raising the question of whether global civilization could ever afford it. Referencing a study by the Economist Intelligence Unit, Joe argues that humanity may not have a choice: climate-induced droughts, floods, crop failures, and supply-chain breakdowns are projected to cost the global economy upwards of $7.9 trillion by 2050. Spending money on mitigation directly injects capital into businesses, payrolls, and working households, rather than burning value on disaster relief. Just as with big planetary missions like Curiosity or Perseverance, money spent on space programs is not simply fired into the void; it circulates through industries, engineers, and local economies.
Even so, building a sunshade is a centuries-long engineering endeavor that acts merely as a temporary temperature band-aid. It does nothing to halt other consequences of greenhouse gases, such as ocean acidification. While spin-off technologies like autonomous robotics, AI, and lunar freight networks would transform human capability, banking on international unity remains historically unrealistic. Joe jokes about the idea of all nations, creeds, and ideologies coming together in selfless sacrifice, only to catch himself:
> “I'm sorry, I'm sorry, I forgot what year we're in.”
---
[24:17](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1457s) Roger Angel’s Verdict: A Distraction from the Real Solution
Even Roger Angel concluded that sunshades should not be treated as a primary escape hatch. Diverting trillions of dollars to manufacture orbital umbrellas while continuing to pump fossil fuels into the atmosphere is fundamentally flawed. Quoting Angel's original paper, Joe highlights the author's own warning against treating geoengineering as a primary fix:
> “The same massive level of technology innovation and financial investment needed for the sunshade could, if also applied to renewable energy, surely yield better and permanent solutions.”
Reflecting on 2020 as a turbulent year of transition marked by the global pandemic, Joe acknowledges that climate change often slips from immediate focus when immediate emergencies dominate. However, rebuilding post-crisis economies presents an opportunity to overhaul the energy grid directly. Investing massive sums into clean terrestrial infrastructure accomplishes economic stimulus while simultaneously tackling emissions at the source—killing two birds with one stone, rather than relying on orbital science fiction.
[25:40](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1540s) Finding Your Passion: Elle Luna and Skillshare
Wrapping up the climate and sunshade discussion, Joe playfully invites viewers to debate in the comments or “throw some shade” at him. Laughing off potential criticism, he explains that doing what he loves keeps him grounded: “I said throw some shade at me, and you know what, I can take it, you know why? Because I love making these videos—this is what I'm passionate about, that makes me immune to your hate.” For viewers looking to connect with their own drive, he recommends the Skillshare course *Choose Must: 10 Exercises to Find and Pursue Your Passion*, taught by artist, designer, and author Elle Luna.
Joe notes that Luna’s philosophy has influenced his channel for years, ever since he first learned about her book through Tim Ferriss. He explains that life often traps people in a web of obligations: “She talks about how we all have our shoulds in life—the things that we have to do to pay our bills and to keep things going and whatnot—but it also means that we kind of reject the other side of the coin, which is our must.” While the “shoulds” represent duty, the “must” represents the deeper calling that provides fulfillment and purpose. Luna’s class translates the concepts from her book into ten practical, step-by-step exercises to help students uncover and execute those goals.
Broadening out to the platform itself, Joe highlights Skillshare’s library of thousands of expert-led courses spanning graphic design, marketing, business essentials, video production, and cooking. He pitches a special promotion where the first 1,000 viewers to register using the link in the description receive two months of Skillshare Premium for free, followed by an ongoing subscription rate under $10 a month, which he calls a far smarter investment than many everyday purchases.
- **Featured Course**: *Choose Must: 10 Exercises to Find and Pursue Your Passion* by Elle Luna - **Key Concepts**: Balancing practical life obligations ("shoulds") against core creative and personal callings ("musts") - **Promotional Offer**: 2 free months of Skillshare Premium for the first 1,000 sign-ups, followed by a membership rate under $10/month
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[27:44](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1664s) Community Support and Channel Sign-Off
Joe shifts to thanking his supporters on Patreon, affectionately called the "Answer Files," who help keep the channel running: “And a huge shout-out to the Answer Files on Patreon that are building a community, supporting the channel, and just being generally overall awesome people.” Before signing off, he takes a moment to read off and welcome a new batch of patrons, joking self-deprecatingly that he will probably mispronounce their names in the process.
He outlines the perks available to supporters who join the community at patreon.com/answerswithjoe, including early access to upcoming videos and direct interaction with him. Finally, Joe directs newcomers to algorithm-recommended videos on the channel, invites viewers to like, share, and subscribe for new weekly uploads, and concludes with his signature farewell: “All right, that's it for now, you guys go out there, have an eye-opening week, be safe, and I'll see you next Monday.”
- **New Patreon Members Acknowledged**: Libby Holtmann, Lauren Newman, Jackie Donnelly, Theodore Wilson, John Pennington III, Donald C. Klein, Peter Pernu, Dean McManus, The Ratty Show, Lance Faye, Alicia Herberter, Chris Leon, Joe In A Box, Jonathan Paul, Kerry Silko, and Jared Danielson - **Upload Schedule**: New episodes published every Monday
## Notable quotes > [24:17](https://www.youtube.com/watch?v=6yqi0FabHHs&t=1457s) The same massive level of technology innovation and financial investment needed for the sunshade could, if also applied to renewable energy, surely yield better and permanent solutions. — Roger Angel
## Mentioned Joe Scott, Roger Angel, Ethan Siegel, Kimi Talvitie, Tim Dodd, Elle Luna, Tim Ferriss, John Thompson, Elon Musk, Skillshare, SpaceX, Starship, Saturn V, New Glenn, Space Launch System, James Webb Space Telescope, Starlink, Proceedings of the National Academy of Sciences, Starts With A Bang, Economist Intelligence Unit, NASA, Eagleworks, EmDrive, Curiosity, Perseverance, The Matrix, Patreon
## Video description The first 1000 people to sign up at https://skl.sh/joescott15 will get 2 free months of Skillshare Premium for free! Space shades are often touted as our last hope if our climate change situation gets too out of control. If we can't keep carbon emissions down, we could just block the sun. I hear this option get thrown out very casually, but I've never seen a realistic look at what that would look like. How big would it need to be? How much would it cost? Wound it even work? So I decided to take a serious deep dive.
Here's the link to the paper by professor Roger Angel: https://www.pnas.org/content/103/46/17184
Animations and shade designs by Kimi Talvitie: Find more of his work on Twitter: @kimitalvitie
Ethan Siegel's take on Starts With A Bang: https://medium.com/starts-with-a-bang/ask-ethan-can-we-build-a-sun-screen-to-combat-global-climate-change-c6399f279ef
Watch this video ad-free on Nebula: https://nebula.tv/videos/joe-scott-sun-shades-wont-save-us-from-climate-change
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[Source](https://www.youtube.com/watch?v=6yqi0FabHHs)