normally butters Ars Praefectus
18y
5,207
Control Group said:
Having never heard of Impulse before, I'd love an explainer of their engineering. What makes their system better at in-space maneuvering?
The previous answers are all good, but I'll add that there are historical reasons why liquid kick/deploy stages have seen little investment in the West until recently, whereas the Soviets developed stages like Fregat and Briz which are conceptually similar to Impulse's Mira.

The US invested heavily in upper stages like Centaur which solve the relatively difficult problem of a high-performance cryogenic stage capable of multiple in-flight restarts. Questionable plans to put Centaur inside the Space Shuttle payload bay were abandoned after the Challenger disaster and replaced with a couple of barely-adequate solid-propellant kick stages for payloads going beyond LEO.

The Europeans, meanwhile, took advantage of their near-equatorial launch site in French Guiana to develop launch vehicles optimized for GEO missions with upper stages inserting into GTO directly from the ascent burn, without requiring any restart. Ariane 5 literally doubled down on this concept of operations by specializing in dual-satellite GTO injection missions. In more modern times, Vega has a liquid kick stage, AVUM, but powered by a hypergolic engine of Soviet heritage which was until recently manufactured in Ukraine.

On the US-headquartered side, Rocket Lab's Electron requires a kick stage from their Photon product line for any orbital mission, once again largely to avoid the challenge of restarting cryogenic stages in microgravity. Firefly, in contrast, has developed a restartable second stage, and they are developing a line of orbital transfer stages based on lower-thrust electric propulsion.

So, Impulse Space just doesn't have much competition in this part of the world. Different approaches were taken to the design of expendable upper stages. But in a future with reusable upper stages that don't want to accelerate to higher energies than they need to, separate kick stages are increasingly compelling. Likewise, if military forces begin to see earth orbit as a more kinetic or dynamic combat theater, that would also encourage kick/transfer stage development, for better or worse. //

Chuckgineer Ars Centurion
10y
323
Subscriptor
Bruce Dunn said:
The Mira thrusters are undoubtably pressure fed. With hydrazine, pressure is provided by helium from composite overwrap pressure vessels through often trouble-prone valves. Impulse does not say how the Mira propellants are pressurized, but it is notable that they both have high vapor pressures at near ambient temperatures. I suspect that the propellants are self pressurized, eliminating the mass and complexity of helium pressurization. At 273 K, the vapor pressure of ethane is 2.4 MPa and that of nitrous oxide is 3.2 MPa.

Hi Bruce, the article above (Industry Update: Prevalance of Nitrous-Based In-Space Propellants) verifies your suspicion: "Nitrous and propylene are self-pressurizing and do not require pumps, pressurants or even propellant management devices."
https://www.dawnaerospace.com/latest-news/prevalence-of-nitrous-based-in-space-propellants