top of page

PAST PROJECTS

EngineTest.png

Upper Stage Rocket Engines

These engines used a novel propulsion system architecture intended to enhance the profitability of space launch systems through a reduction in system cost, complexity, and development schedule. The engines were capable of scaling over a wide thrust range. Performance approached pump-fed systems with lower complexity than traditional pressure-fed systems.

In-Space Thrusters

Using the same core technology of the larger upper stage engine, these thrusters were designed to bring high performance propulsion to spacecraft, kick stages, OTVs and landers.

​

​

Sounding Rocket

The K-200 was a single stage liquid propellent sounding rocket. Utilizing the previously developed  propulsion system, the elegant architecture reduces complexity and cost of traditional propulsion technologies. This allowed for a small and high-performance vehicle capable of being rapidly deployed and launched at any remote location.

© 2024 by Snowdon Consulting Limited

    bottom of page