Thunderf00t
SpinLaunch's $100 million centrifuge reproduces 1960s Project HARP artillery at inferior speeds and higher mechanical strain, while unpowered atmospheric deceleration leaves its liquid rocket engines starved of fuel.
AI-assisted summary of Spinlaunch: BUSTED (Part 2) — original source. Check the original for full context.
Source published:
Key ideas
- Thunderf00t challenges SpinLaunch's launch physics, showing that unpowered atmospheric ascent forces liquid propellants away from engine feed lines without dedicated ullage motors to settle them. (0:00)
- Rotational kinematics on SpinLaunch test footage reveal a tip speed of roughly 300 m/s (around Mach 1), directly contradicting claims of tests exceeding Mach 6. (2:53)
- SpinLaunch's long-term targets of hurling 200 kg at 2,000 m/s fail to outperform the 1960s Project HARP supergun, which achieved the same velocity with lower peak acceleration and without subjecting payloads to an hour-long spin-up. (10:58)
- Operational requirements such as an 8-hour vacuum pump-down make SpinLaunch drastically slower to refire and far more vulnerable to catastrophic structural failure than conventional or historical artillery. (4:33)
Detailed notes
## Background Published on YouTube by Thunderf00t on November 24, 2021, this video is the second installment in his series debunking the kinetic space launch startup SpinLaunch. The accompanying video description directs viewers to support his work via Patreon, browse his Amazon affiliate storefront, or visit his secondary channel.
## TL;DR Thunderf00t breaks down the severe engineering and physics shortcomings behind SpinLaunch's rotational orbital accelerator. He explains that an unpowered projectile decelerating through dense atmosphere pushes liquid propellant away from engine feed lines due to the lack of ullage thrusters, and he uses rotational kinematics to demonstrate that SpinLaunch's test centrifuge attained only roughly Mach 1 rather than the advertised Mach 6. Finally, he compares the concept to century-old naval guns and 1960s supergun initiatives like Project HARP, arguing that SpinLaunch is spending over $100 million to build a more fragile, slower-firing, and technically inferior version of technology proven over half a century ago.
## Atmosphere & style The presentation carries an acerbic, biting, and relentlessly sarcastic tone characteristic of Thunderf00t's debunking videos. Fast-paced mathematical calculations and frame-by-frame video dissections are paired with dry mockery of startup culture, Silicon Valley hype, and uncritical tech journalism. The viewing experience feels like a methodical intellectual dismantling, juxtaposing polished CGI marketing animations against the unyielding physical realities of fluid dynamics and heavy artillery history.
## Bulletin - [00:00](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=0s) Thunderf00t challenges SpinLaunch's launch physics, showing that unpowered atmospheric ascent forces liquid propellants away from engine feed lines without dedicated ullage motors to settle them. - [02:53](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=173s) Rotational kinematics on SpinLaunch test footage reveal a tip speed of roughly 300 m/s (around Mach 1), directly contradicting claims of tests exceeding Mach 6. - [10:58](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=658s) SpinLaunch's long-term targets of hurling 200 kg at 2,000 m/s fail to outperform the 1960s Project HARP supergun, which achieved the same velocity with lower peak acceleration and without subjecting payloads to an hour-long spin-up. - [04:33](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=273s) Operational requirements such as an 8-hour vacuum pump-down make SpinLaunch drastically slower to refire and far more vulnerable to catastrophic structural failure than conventional or historical artillery.
## Key takeaways - [00:00](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=0s) SpinLaunch relies on liquid-fueled engines, but unpowered ascent causes rapid deceleration that pushes propellant to the top of the tanks and starves the engines without ullage motors. - [02:53](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=173s) Video analysis of the 30-meter centrifuge test indicates roughly 3 revolutions per second, equating to ~300 m/s (Mach 1) rather than the claimed Mach 6 or 'thousands of miles per hour'. - [04:33](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=273s) Century-old 16-inch naval guns fired 1-ton shells at Mach 2.5 to 3.0 every 30 seconds, demonstrating roughly 50,000 times higher cumulative launch energy than SpinLaunch's subscale test. - [04:33](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=273s) SpinLaunch requires an estimated 8 hours to draw a vacuum to avoid catastrophic aerodynamic heating during spin-up, resulting in an extremely poor launch cadence. - [06:48](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=408s) While artillery impulses subject payloads to extreme g-forces for fractions of a second, SpinLaunch subjects electronics and mechanisms to sustained 10,000+ g acceleration for nearly an hour. - [06:48](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=408s) Historical systems like Cold War atomic artillery shells prove delicate guidance and timing electronics can survive short, high-g cannon launches. - [06:48](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=408s) Extended barrel designs, from the German WWII V-3 multi-chamber gun to Project HARP, demonstrate that prolonged barrel acceleration effectively manages peak g-forces. - [10:58](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=658s) In the 1960s, Project HARP fired 200 kg projectiles at ~2,000 m/s under 15,000 g's, matching or exceeding SpinLaunch's projected Mach 7 performance using low-cost welded battleship barrels. - [10:58](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=658s) SpinLaunch openly references Project HARP in its promotional materials, effectively advertising that it is attempting an inferior and costlier replica of 50-year-old technology. - [13:00](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=780s) Artillery engineer Gerald Bull adapted Project HARP concepts into Saddam Hussein's Project Babylon supergun before his assassination and the project's interception. - [14:20](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=860s) Centrifuges carry catastrophic failure risks where any imbalance or tether break at hypersonic speed destroys the entire facility, whereas gun barrels are inherently durable. - [15:37](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=937s) Thunderf00t concludes by previewing an upcoming debunk of a viral 'solid hydrogen at room temperature' energy startup claim.
## Detailed walkthrough ### [00:00](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=0s) The SpinLaunch Concept and the Ullage Problem
Thunderf00t revisits SpinLaunch for a second debunking video after taking a step back and realizing foundational physics do not add up. He summarizes the company's origin story with heavy sarcasm: a founder with zero background in rocketry or satellites simply wondered how to revolutionize space launches, asked whether payloads could reach orbit without a traditional rocket, and arrived at the concept of a rotational accelerator. Thunderf00t quips that while one might expect breakthrough aerospace concepts to originate from seasoned engineers, this was just an everyday individual whose napkin idea suddenly became a $100 million startup—joking that had he adopted a deep voice, donned a black turtleneck, and claimed to be a Harvard dropout, it would have been a $9 billion startup like Theranos.
The sleek computer-generated imagery (CGI) portrays a seamless launch sequence: the machine spins like an enormous trebuchet, flings a projectile out of a sealed vacuum chamber, and the rocket engine kicks in to push it into orbit. But as Thunderf00t emphasizes, real physics breaks this fantasy immediately. The proposed vehicle utilizes liquid-fueled engines, visible by its fuel and propellant tanks. Liquid rocket engines require continuous settling pressure to force liquid propellant toward the bottom feed lines and pumps.
Because the flung projectile is unpowered during its initial ascent, it decelerates violently due to atmospheric drag. This deceleration forces the fuel upward against the front dome of the tank rather than toward the engine feed lines at the bottom. Standard rocketry solves this issue through ullage motors—small auxiliary thrusters fired briefly to generate forward acceleration, settling liquid propellant prior to main engine ignition. While SpinLaunch’s animation depicts a small motor to de-spin the projectile, it lacks any ullage motors entirely. Thunderf00t points out:
> “Except that's not how physics work 100 percent that's not how physics work you see you know these are liquid fed engines because you can see the fuel and the propellant tank so in order to actually pump the stuff out of there you need a force pushing it to the bottom of the tanks but wait this yiking machine is dumbfire these projectiles are unpowered which means they're always slowing down due to the atmospheric drag.”
```mermaid flowchart TD accTitle: The Ullage Problem in Flung Liquid Rockets accDescr: Diagram contrasting fuel positions at rest on the ground versus during unpowered atmospheric ascent, highlighting engine starvation.
subgraph Ground["At Rest on Ground"] G1["Fuel sits at bottom of tank"] --> G2["Feeds normally into engine lines"] end
subgraph Ascent["Unpowered Ascent through Atmosphere"] A1["High atmospheric drag causes rapid deceleration"] --> A2["Fuel sloshes against front of tank"] A2 --> A3["Engines starved of propellant"] A3 -.->|"Required fix omitted by SpinLaunch"| A4["Ullage motors needed to settle fuel"] end ```
[02:53](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=173s) Debunking SpinLaunch's Velocity Claims
Thunderf00t addresses official claims regarding launch speeds. SpinLaunch’s website FAQ asserted that their orbital accelerator spins up to roughly 5,000 miles per hour prior to release and claimed to have conducted tests exceeding six times the speed of sound (Mach 6). CNBC similarly echoed these figures, reporting test velocities reaching "many thousands of miles per hour using approximately 20 percent of the accelerator's power capacity."
Thunderf00t verifies these claims using basic rotational kinematics on their test centrifuge footage: - The centrifuge chamber measures roughly 30 meters in diameter, giving a circumference of approximately 100 meters. - Audio from the test clip is accompanied by an artificial Doppler whoosh sound effect, despite the arm ostensibly spinning inside an evacuated vacuum chamber. - Frame-by-frame analysis with a timecode shows the arm takes approximately 0.33 seconds per full rotation (or roughly two complete rotations in 0.6 seconds), establishing a rotational rate of roughly 3 revolutions per second. - Multiplying a 100-meter circumference by 3 revolutions per second yields a linear tip speed of roughly 300 meters per second.
This puts the tested speed around Mach 1 (the speed of sound) or roughly 670–700 mph, completely contradicting claims of Mach 6 or "many thousands of miles per hour." Thunderf00t calls out the discrepancy plainly:
> “To date we've conducted tests at over six times the speed of sound this is straight out I mean you know the size of the centrifuge it's about 30 meters in diameter which means it's about 100 meters around the outside so let's count how many revolutions this thing's doing per second.”
[04:33](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=273s) SpinLaunch vs. Century-Old Battleship Cannons
Thunderf00t compares SpinLaunch's performance to century-old naval artillery technology: 16-inch heavy battleship guns. During their operational prime, battleship guns delivered pinpoint accuracy over horizons beyond 20 miles (even when deck observers could only see 14 miles), firing 1-ton explosive shells at standard muzzle velocities of Mach 2.5, or up to Mach 3 when heavily charged. By contrast, SpinLaunch releases its test projectile at roughly the speed of sound with dubious exit stability, visibly tipping around 30 degrees off-axis upon exiting the vacuum seal chimney.
Operational turnaround times highlight an even wider gap. The SpinLaunch chamber requires a near-complete vacuum before spinning up to prevent catastrophic aerodynamic drag and overheating on the tether arm, taking an estimated 8 hours to pump down between launches. A standard battleship gun fires two shells per minute per barrel (one every 30 seconds)—over 1,000 times faster.
| Metric | Century-Old Battleship Gun (16-Inch) | SpinLaunch Test / Projections | Advantage Factor | |:--- |:--- |:--- |:--- | | **Muzzle Velocity** | Mach 2.5 to 3.0 (~850–1000 m/s) | Mach 1 tested (~300 m/s) | Gun is ~3× faster | | **Projectile Mass** | ~1,000 kg (1 ton) | ~200 kg (proposed missile) | Gun is ~5× heavier | | **Kinetic Muzzle Energy** | Extreme ($E_k = \frac{1}{2}mv^2$) | Low compared to projectile weight | Gun is ~50× higher energy | | **Firing Cycle / Cadence** | 1 round every 30 seconds (2/min) | ~8 hours pump-down time | Gun is ~1,000× faster | | **Cumulative Capability** | Rapid-fire salvo capability | Single experimental release | Gun is ~50,000× superior overall |
Thunderf00t emphasizes how poorly SpinLaunch stacks up against century-old technology:
> “Now you stack all the irrelevant practice here and spin launch is some fifty thousand ish times worse than a regular battleship gun in terms of how much energy it can launch so you see already in the comparison to a gun not designed for this purpose spin launch has an awful lot of catching up to do.”
[06:48](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=408s) Sustained G-Forces, Gun-Launched Nukes, and the V-3 Cannon
Thunderf00t addresses the counterargument regarding peak acceleration: does firing electronics from a cannon destroy delicate components compared to a centrifuge? While both subject payloads to extreme peak loadings (often topping 10,000 g), a cannon impulse lasts only a fraction of a second during barrel travel. In contrast, SpinLaunch subjects delicate payload electronics and folded mechanisms to these crushing loads continuously over roughly an hour as the centrifuge slowly spins up to speed.
To illustrate how high-g gun launches can accommodate delicate hardware, he cites the US military's Cold War atomic artillery shells (such as the M65 atomic cannon). A nuclear weapon requires precise timing circuits and shaped explosive lenses to implode plutonium cores properly, yet engineers designed functional gun-fired nuclear shells.
Examining famous archival footage of the M65 atomic cannon test, Thunderf00t dissects the film's timing. Based on a muzzle velocity of Mach 2 (~600 m/s or 2 km every 3 seconds) firing toward a target roughly 10 kilometers away, the flight time must be around 15 seconds, followed by an additional 30 seconds for the blast's sound wave to travel back to the battery. In widely circulated documentary clips, the detonation appears only 7 seconds after firing, and smoke from the cannon vanishes abruptly due to an edit. Finding uncut historical footage, he reveals the narrator awkwardly stalling through an explanatory sentence across the 15-second flight gap before the fireball finally erupts on the horizon.
Thunderf00t notes that using extended propulsion inside a barrel to reduce peak g-forces dates back even further. During World War II, Germany deployed three *Vergeltungswaffen* (Vengeance weapons): - The V-1 flying bomb (powered by an atmospheric pulsejet engine) - The V-2 ballistic rocket - The V-3 supergun
Standard guns experience peak chamber pressure at initial ignition, which drops rapidly as the projectile travels down the barrel. The V-3 supergun was engineered as a multi-chamber accelerating gun, employing sequential propellant charges along the length of the barrel timed to detonate just behind the moving shell to sustain acceleration.
[10:58](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=658s) Project HARP and the $100M "Worse Copy"
Thunderf00t examines the physics of artillery and gun-based launch systems, noting that instead of detonating sequential secondary charges along a barrel, engineers can use slower-burning propellants that sustain pressure behind the shell. Under this design, final muzzle velocity is directly dictated by barrel length: the longer the barrel, the greater the acceleration. This principle was fully demonstrated in the 1960s by Project HARP (High Altitude Research Project). Thunderf00t points out the profound irony that SpinLaunch openly references Project HARP in their own promotional materials, calling the comparison a massive self-inflicted wound because it instantly exposes how unoriginal and inferior SpinLaunch’s core concept is.
When looking at the actual performance figures, SpinLaunch’s aspirational targets fail to improve upon a project carried out half a century earlier. SpinLaunch claims it will hurl a 200-kilogram projectile at roughly 5,000 miles per hour (around 2,000 meters per second, or Mach 7), subjecting the payload to peak forces of approximately 20,000 g’s. Decades ago, Project HARP accomplished virtually the exact same feat: firing a 200-kilogram shell at roughly 2,000 meters per second. However, HARP subjected its payload to a lower peak load of 15,000 g’s, and that acceleration took place for merely a fraction of a second inside a rigid tube, rather than forcing delicate space hardware to endure an hour of continuous mechanical stress inside a spinning centrifuge.
As Thunderf00t summarizes the comparison: “I mean you can imagine the second people look into this they find out that the entire sales pitch of spin launch is we're going to be 100 million dollar startup that is going to make a worse copy of something that was done 50 years ago.”
- **SpinLaunch targets:** ~200 kg projectile, ~5,000 mph (~2,000 m/s / Mach 7), ~20,000 g maximum load, accelerated over 60 minutes in a centrifuge. - **Project HARP achievements:** ~200 kg projectile, ~2,000 m/s, ~15,000 g load, accelerated over a fraction of a second inside a barrel.
[13:00](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=780s) The Iraqi Supergun, Gerard Bull, and Battleship Barrels
Unlike a massive vacuum centrifuge that takes an hour to spin up to launch speed, conventional gun systems can fire repeatedly as quickly as fresh rounds are loaded into the breech. Thunderf00t emphasizes that Project HARP was effectively a low-cost, "bargain basement" endeavor, constructed simply by welding two surplus 16-inch naval battleship gun barrels end-to-end to create a single ultra-long launch tube.
The supergun concept was famously pursued decades later by Iraqi dictator Saddam Hussein under Project Babylon, designed by Canadian artillery engineer Dr. Gerald Bull—the very same engineer behind Project HARP. The Iraqi gun components were manufactured in the United Kingdom out of top-grade Sheffield steel, disguised as oversized petrochemical reactor pipes. Customs officials eventually intercepted the curiously straight, heavily over-engineered steel tubes because they lacked any standard petrochemical fittings, and Bull was subsequently assassinated in Brussels in 1990. While Hussein built a smaller prototype with range comparable to the German V-3 cannon and planned an orbital-class gun of virtually unlimited range, fixed superguns suffered from the fatal military flaw of being completely immobile and un-aimable, outside of modest aerodynamic steering surfaces on the projectile itself.
As Thunderf00t observes: “And the only people I know who seriously revisited the idea of the super gun since was Saddam Hussein with the Iraqi super gun made in Britain.”
[14:20](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=860s) Reality vs. Aspiration: Why SpinLaunch Fails Against 1960s Tech
Gun-launch technology capable of achieving hypersonic speeds has existed for over fifty years. Thunderf00t stresses that the SpinLaunch centrifuge attempts to duplicate the exact same operational profile, yet scores worse across every meaningful engineering metric. Crucially, Project HARP was a proven piece of hardware that actually operated in physical reality, whereas SpinLaunch’s published milestones are merely aspirational targets promoted by a startup founder without a background in the field. SpinLaunch’s sub-scale prototype tests have yet to even surpass the velocity of ordinary military artillery.
The operational drawbacks of a centrifuge system are severe. Achieving hypersonic speeds at sea level requires pumping down a massive chamber to a high vacuum so the tethered payload does not burn up from atmospheric friction during its hour-long spin-up, resulting in an abysmal refire rate. Furthermore, the structural risks are catastrophic: any mechanical failure, tether break, or unbalance at hypersonic velocity will instantly obliterate the entire centrifuge building. By contrast, Project HARP relied on an inherently rugged, low-cost piece of equipment: what Thunderf00t characterizes as nothing more complex than a "big thick metal straw."
As Thunderf00t puts it: “The centrifuge essentially does exactly the same thing but is worse on any comparable metrics with probably the most important one being is that project harp actually existed.”
| Metric / Feature | Project HARP (1960s) | SpinLaunch (Projected) | |:--- |:--- |:--- | | **Projectile Mass** | ~200 kg | ~200 kg | | **Launch Velocity** | ~2,000 m/s (~5,000 mph) | ~2,000 m/s (~5,000 mph) | | **Peak Acceleration** | ~15,000 g | ~20,000 g | | **Acceleration Duration** | Fraction of a second | ~60 minutes | | **Cycle / Refire Time** | Minutes (limited only by reloading) | Hours (vacuum pumpdown + 1 hr spin-up) | | **Core Architecture** | Two bolted 16-inch battleship barrels | Massive evacuated centrifuge chamber | | **Failure Vulnerability** | High structural barrel tolerance | Catastrophic facility destruction |
```mermaid flowchart TD accTitle: SpinLaunch vs Project HARP Launch Cycle accDescr: Operational flowchart comparing the rapid, robust firing cycle of Project HARP to the slow, highly vulnerable centrifuge process of SpinLaunch.
subgraph HARP ["Project HARP (Supergun)"] H1["Load 200 kg projectile"] --> H2["Ignite propellant charge"] H2 --> H3["Hypersonic exit in fraction of a second"] H3 --> H4["Immediate reload and repeat"] end
subgraph SPIN ["SpinLaunch (Centrifuge)"] S1["Evacuate chamber to deep vacuum"] --> S2["Spin tethered rocket for ~1 hour"] S2 --> S3["Release through launch tunnel"] S3 --> S4["Slow chamber repressurization & pumpdown cycle"] S2 -.->|"High-speed mechanical failure"| S5["Total destruction of launch facility"] end ```
[15:37](https://www.youtube.com/watch?v=ibSJ_yy96iE&t=937s) Teaser: The "Solid Hydrogen" Scam
Thunderf00t wraps up his analysis of SpinLaunch by tongue-in-cheek noting that, whatever its flaws, SpinLaunch at least never claimed its technology was suppressed by authorities. He previews his next debunking subject: a viral promotional video for an energy startup claiming to store hydrogen as a solid at ambient conditions, complete with the claim that the technology is "so good that it was actually banned."
Thunderf00t lambasts the premise as pure scientific illiteracy, emphasizing that solid hydrogen requires temperatures near absolute zero and noting that the concept makes SpinLaunch look like a well-reasoned enterprise by comparison. He urges viewers to subscribe and support the channel on Patreon to catch the upcoming debunking breakdown.
Regarding the upcoming target, Thunderf00t delivers a biting critique: “And spoiler this is one of the most scientifically illiterate videos that I've ever seen and I debunk creationists.”
## Mentioned Thunderf00t, SpinLaunch, Theranos, CNBC, M65 atomic cannon, V-1 flying bomb, V-2 rocket, V-3 supergun, Project HARP, Gerald Bull, Project Babylon, Saddam Hussein, Patreon
## Video description You can support this channel directly through patreon: https://patreon.com/Thunderf00t
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or my other channel: https://www.youtube.com/channel/UCUrdmVprSahXaPKqr04VfgQ
[Source](https://www.youtube.com/watch?v=ibSJ_yy96iE)