超高速客运的未来
The future of ultra-fast passenger travel

原始链接: https://spaceambition.substack.com/p/beyond-the-sound-barrier

## 超音速和超高音速旅行的回归:风险投资者的视角 超音速客运飞行的梦想正在复苏,初创公司(如Boom、Hermeus)和航空航天巨头都在追求超过马赫1的速度。尽管协和式飞机因高成本和限制而失败,但材料、推进(如冲压发动机/超燃冲压发动机)和可持续燃料方面的进步提供了潜在的解决方案。 然而,速度是有代价的:燃料效率会随着马赫数的增加而*急剧下降*。超音速和超高音速旅行本质上需要更高的每乘客-英里燃料消耗,从而影响成本和排放。有趣的是,弹道亚轨道旅行,例如SpaceX的星舰,可能具有令人惊讶的竞争力,尽管发射成本高昂,但可以最大限度地减少飞行*期间*的燃料消耗。 最初的市场不会是大众旅行。超快速飞行可能到2030年瞄准一个价值300-600亿美元的利基市场——愿意支付4000-10000美元以上机票的高端商务旅客和豪华游客。仍然存在重大的资金缺口,并且需要解决监管障碍(如超音速轰鸣限制)。投资具有风险,需要长期的眼光,但双用途技术和潜在的监管变化为成功提供了途径。

## 超高速旅行的未来:黑客新闻讨论 一篇关于超高速客运的文章在黑客新闻上引发了争论,主要集中在超音速飞行面临的经济和实际挑战。尽管快速跨越大陆的梦想依然存在,但许多评论员质疑其可行性。 讨论着重强调了协和式飞机的失败,认为其原因并非仅仅是法规(音爆限制),还包括其高昂的成本、噪音水平以及作为冷战时期缺乏美国参与的声望项目。人们对环境影响表示担忧——更高的燃油消耗和排放,以及这种旅行是否真的能服务于除超级富豪以外的任何人。 有人提出了替代方案,例如高速铁路以及更舒适、更慢的旅行体验(例如豪华火车旅行)。一些人认为,专注于改进现有的旅行方式并优先考虑可及性,比追求小众且昂贵的解决方案更有益。另一些人设想未来快速旅行可以带来好处,例如更快的器官运输和更强的全球合作,但也承认了潜在的缺点,例如疾病传播加速。最终,共识倾向于对广泛的超音速旅行持怀疑态度,许多人认为经济现实和实际限制将占据上风。
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原文

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The charm of supersonic passenger travel didn't end with Concorde's retirement in 2003. Today, aerospace startups and giants alike chase ambitious dreams of passenger flights that exceed the speed of sound, connecting continents in mere hours or even minutes. But what does this resurgence mean for venture investors?

By the way, it’s no coincidence aviation shows up in our spacetech blog — ultra-fast passenger travel is exactly where aero and space intersect in a meaningful way.

Concorde, cruising at twice the speed of sound (Mach 2), ultimately failed economically due to excessive operating costs, poor fuel efficiency, and regulatory restrictions on overland supersonic flights. Today's aerospace startups argue that new materials, advanced propulsion, and sustainable fuels can overcome these historical challenges.

The speed of a vehicle in flight is usually expressed as a Mach number: the ratio between its true air speed and the local speed of sound (≈ 343 m/ s at sea level). Speeds between Mach 1 and Mach 5 define supersonic flight, while Mach 5 and above is considered hypersonic. Higher speeds generally require higher altitudes because thinner air reduces aerodynamic drag and heating.

At the extreme end, rockets avoid drag almost entirely once they are above ~50 km. Ballistic sub‑orbital (“Earth‑to‑Earth” or “Point‑to‑Point”) trajectories, like SpaceX’s Starship concept, momentarily reach ~ Mach 20 outside the sensible atmosphere before re‑entering on a purely ballistic arc. Including ballistic rockets as the “limit case” is therefore useful: they show what happens when you remove all cruise drag but pay a very large propellant cost during ascent and landing.

High-speed travel introduces significant technological challenges.

Modern high‑bypass turbofan engines used by commercial aircraft move a large mass of “slow” air for high propulsive efficiency. The bypass stream goes to the fan, and may be 10 kg of air for every 1 kg through the core, where it mixes with the fuel and burns. Above about Mach 0.95, that big and slow fan becomes a wall of drag, and the fan blades encounter supersonic flow. Therefore, engineers revert to much smaller, low‑bypass cores or entirely different cycles (ramjet/scramjet) that work only when the vehicle itself compresses the air thanks to its high speed:

In recent decades, aviation prioritized fuel efficiency over speed, transitioning to turbofan engines with increasingly higher bypass ratios. Higher bypass means engines use a larger amount of air relative to fuel combustion products, significantly improving fuel efficiency (specific impulse) at subsonic speeds but unsuitable for supersonic travel.

Consequently, both supersonic and hypersonic travel naturally require more fuel per passenger-mile compared to subsonic flights, leading to increased operating expenses and environmental impact. Quantitatively, the picture looks like this:

  • A Boeing 787‑10 in dense layout consumes 1.3 kg/100 km/passenger. The corresponding specific impulse Isp is ~ 12,000 s. Let us remind that Isp is inversely proportional to fuel used per unit of time. Compare it to a typical chemical rocket engine (Merlin) with its 350 s. The high specific impulse of Boeing 787 does not mean that it translates to 120,000 m/s (10x of Isp) exhaust speed, as it would be with a non-air-breathing rocket engine. It means that even with moderate exhaust speeds (417 m/s), thanks to the air trapped by the fan, fuel is a small fraction of the overall exhaust. Pushing extra mass of ambient air instead of hot exhaust cuts fuel consumption significantly;

  • Concorde managed ≈ 10.3 kg/100 km/passenger of fuel consumption. The corresponding specific impulse is 3,000 s;

  • Hypersonic aircraft have even lower specific impulse than Concorde, somewhere in the range between 1,000 and 2,000 s;

  • From the point of view of Isp, rockets perform the worst of all, about 10x worse than supersonic aircraft and 35x worse than subsonic aircraft. But rocket-based ballistic travel concepts like SpaceX's Starship differ economically. Though rockets have an order of magnitude smaller specific impulse and use substantial fuel at launch, they require no fuel during the ballistic trajectory, experiencing minimal air drag at extreme altitudes. So, which side of the tradeoff will prevail: the massive fuel consumption caused by engine inefficiency, or the potential fuel savings from smooth, low-resistance ballistic flight through space? Detailed analysis suggests Starship’s fuel efficiency per passenger-mile could be near 30 kg/100 km/passenger of propellant (methane and liquid oxygen combined), comparable with hypersonic jets, potentially making rocket travel economically viable within luxury and premium tourism segments.

More fuel per seat‑km means higher CO₂ if sustainable aviation fuel (SAF) is scarce. Supersonic NOₓ and water vapour are emitted directly into the lower stratosphere, affecting ozone and radiative forcing. Methalox rockets also inject large quantities of H₂O and NOₓ at >30 km.

As a result, economics forces very fast travel into high‑yield niches—premium business time‑savers, luxury tourism, and government/military missions, rather than mass economy travel.

Boom Supersonic projects ticket prices for its Mach 1.7 "Overture" airliner around $4,000–$5,000, comparable to current transatlantic business-class fares (~6,000 km). However, initial pricing realistically could surpass $10,000 until operational economies of scale are achieved.

The global intercontinental aviation market is enormous—approximately 400 million passengers annually, generating around $600 billion in revenue. Yet, ultra-fast travel initially targets only 2–5% of this market: high-value business travelers and ultra-premium leisure travelers willing to pay premium fares.

Despite supersonic passenger travel could capture a $30–60 billion market by the 2030s, substantial funding gaps remain. Boom has secured roughly $700 million but requires billions more for aircraft certification and mass production.

Regulatory hurdles also remain significant. The current FAA ban on supersonic flights over land restricts market potential to transoceanic routes. NASA’s ongoing X-59 QueSST program aims to demonstrate quieter sonic booms, potentially changing regulations by the late 2020s and opening additional routes.

Investing in ultra-fast passenger travel involves substantial risks but significant potential rewards. Early success hinges on overcoming technological, regulatory, and environmental barriers. Realistically, commercialization remains at least a decade away; initial market niches will likely be premium business and luxury travelers. Dual-use strategies (civilian and military applications), as employed by Hermeus, may mitigate initial investment risks.

While breaking the sound barrier again captivates our imagination, prudent investors must be prepared for a long journey marked by innovation and considerable turbulence.

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