新型卫星引擎可利用地球大气层实现无限期在轨运行
New Satellite Engine Could Use Earth's Atmosphere to Stay in Orbit Indefinitely

原始链接: https://scitechdaily.com/new-satellite-engine-could-use-earths-atmosphere-as-fuel-to-stay-in-orbit-indefinitely/

斯图加特大学的研究人员开发出一种极具前景的“吸气式”等离子推进器,旨在使卫星能够在极低地球轨道(VLEO)长期运行。与依赖氙气等有限机载推进剂的传统发动机不同,该系统能够捕获大气中的气体(如氧气和氮气),并将其转化为等离子体以产生推力。 该项目解决了两个主要的工程难题。首先,为应对原子氧的腐蚀作用,该系统采用了耐用的抛物面反射进气口,能高效地将粒子导入发动机。其次,它采用了一种受核磁共振技术启发的“鸟笼式”天线,用以产生射频螺旋波等离子体射流。这种创新设计产生了一种准中性等离子束,从而无需使用在超高层大气中极易腐蚀的电子中和阴极。 实验室测试证实,该发动机能在极低功率下产生稳定推力。模拟结果表明,这项技术可使卫星在 190 至 250 公里的高度维持永久轨道运行,甚至有望在火星大气中运行。尽管仍需进行任务测试,但这一进展为延长低轨道卫星的使用寿命提供了一条可持续的途径。

最近 Hacker News 上的一场讨论聚焦于一项卫星引擎新技术,该技术能够利用地球大气作为推进剂,从而使卫星有望在极低地球轨道(VLEO)上实现无限期驻留。 尽管评论者们承认 VLEO 卫星推进并非新概念,但他们强调,这项研究的核心挑战及重点在于实际应用,特别是如何克服硬件腐蚀问题。支持者指出,在如此低的高度(约 100 至 250 公里)运行,可以显著提升遥感仪器的分辨率。 然而,社区对该技术的可行性及其广泛影响反应不一。怀疑论者提出了关于极端大气阻力、轨道震动增加以及对高层大气潜在环境影响的担忧。另一些人则认为,“从构思到原型机之间仍存在巨大的鸿沟”,并指出从理论设计转向功能性硬件才是真正的障碍。归根结底,这场讨论突显了将空间技术从概念上的可行性转化为可持续、长期应用所面临的持续挑战。
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原文
Fully Assembled RF Helicon Based Plasma Thruster
Fully Assembled RF Helicon-based Plasma Thruster. Credit: F. Romano

A satellite engine that uses atmospheric gases as fuel shows promise in laboratory tests and modeling, but its performance on a mission remains unproven.

Choosing an orbit for a satellite involves balancing benefits and drawbacks. Very Low Earth Orbit (VLEO), which spans roughly 100 to 450 km (62 to 280 miles) above Earth, offers several advantages. Remote sensing cameras can capture sharper images, communications and radar systems need less power, and atmospheric drag helps remove inactive satellites from orbit naturally.

That same atmosphere also creates a major challenge. Even at these altitudes, air resistance slows spacecraft down, so satellites must produce thrust almost continuously to remain in orbit. Conventional propulsion systems require onboard fuel, often costly gases such as xenon.

As part of his PhD research at the University of Stuttgart, published on arXiv, Francesco Romano explored a different approach. His concept uses the atmospheric molecules responsible for drag as fuel for a plasma engine, potentially allowing satellites to remain in VLEO indefinitely without carrying a conventional supply of propellant.

The technology belongs to a class known as atmosphere-breathing electric propulsion (ABEP). These systems collect the extremely thin air in front of a spacecraft (or, in some cases, a missile) and direct it into an electric engine. The engine converts the incoming molecules into plasma and expels it from the rear to generate thrust.

The basic idea is straightforward, but turning it into a practical propulsion system requires solving several difficult engineering problems.

Atomic oxygen eats away at engines

First is atomic oxygen (AO). In the upper atmosphere, UV radiation splits O2 into this aggressive, single atomic form of the gas that we all need to breathe. AO is notoriously oxidative, corroding metal electrodes, acceleration grids, and even the cathodes used in standard Hall thrusters or other types of ion engines.

Perhaps most importantly, AO burns through the cathodes used in the “electron gun” that neutralizes the spacecraft so that the whole thing doesn’t become charged and simply suck the charged particles right back to itself, nullifying the thrust they provide. Without that feature, the whole ion propulsion system fails.

Another difficult feature when designing engines for use in VLEO is the variability of the atmosphere itself. It changes based on the day/night cycle, the latitude, and even solar activity. Making sure an engine can continually operate in all these different conditions has proven difficult so far.

A mirror that gathers thin air

To solve these problems, Romano developed a contactless, neutralizer-less radio-frequency (RF) helicon plasma thruster and paired it with an optimized atmospheric intake system. Let’s tackle the intake system first.

He actually trialed three different versions of an intake – one called an “enhanced funnel design,” which acted as a molecular trap to capture air particles that are spread so far apart they never run into each other. Next, he used a “diffuse intake” that used a compact hexagonal design made out of a coated titanium alloy. And finally, he designed what he called a “specular intake,” which is a parabolic mirror coated with graphite or silicon dioxide that bounced particles directly into the engine.

The clear winner, both in terms of collection efficiency and alignment sensitivity, was the specular intake. It collected ~94.3% of the particles of air (which was AO, argon, or nitrogen in a wind tunnel test), and the efficiency only dropped by 8% when subjected to a 15° tilt.

Close Up of MRI Inspired Birdcage Antenna
Detailed look at the Birdcage antenna, inspired by MRI machines. Credit: F. Romano

A plasma jet without a neutralizer

To design the thruster, Romano turned to a medical device for inspiration. Using a birdcage antenna, similar to those used in MRIs, he managed to design a thruster that ensured 99% of the delivered electrical power actually entered the thruster, an extremely high-efficiency threshold that improved upon standard wire coils that would burn through some of the power because of their own reactance. A solenoid wrapped around the engine creates a magnetic field that pushes the plasma out the back in a quasi-neutral jet – both positive and negative ions are pushed out of the thruster, ensuring no neutralizer is needed.

Testing the system proved its reliability. Romano used a vacuum chamber to intentionally simulate a VLEO atmospheric concentration of the three primary gases the thruster would encounter at that altitude. The engine generated steady streams of plasma with only 50-60W of RF power, well within the capabilities of traditional spacecraft solar panels.

Could atmospheric fuel keep satellites aloft?

After that experimental validation, he took an additional step and applied models of the propulsion system to actual real-world use cases. This included the GOCE satellite, which famously launched into VLEO with a Xenon ion thruster, and eventually ran out of fuel.

According to the thesis’ calculations, the new engine could operate indefinitely between 190 and 250 km using less than 1.6 kW of power, which is still well within the generation limits of standard spacecraft solar panels. But the use cases aren’t limited to Earth. Mars has an atmosphere dominated by CO2, and, according to the thesis, the engine could support a spacecraft indefinitely above the Red Planet at a height of 120-160 km, which is much closer than existing orbital satellites.

Ultimately, there is no guarantee this thruster will ever see use outside of a lab. But the idea is intriguing, and there are plenty of potential commercial applications for it if it can be de-risked and proven to work on an actual mission. It’s unclear whether Dr. Romano has any plans to pursue that track, but his work on it so far at least shows the design has potential – maybe someone out there is willing to pursue it.

Reference: “RF Helicon Plasma Thruster for an Atmosphere-Breathing Electric Propulsion System (ABEP)” by Francesco Romano, July 1, 2026, arXiv.
DOI: 2607.02635

Adapted from an article originally published in UniverseToday.

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