Flight Works, Inc. — National Aeronautics and Space Administration SBIR Phase I: Z8
Flight Works, Inc. — SBIR Phase I award from National Aeronautics and Space Administration.
Phase I SBIR feasibility signal
- Phase I awards fund proof-of-concept work. For capture teams, they mark early interest from National Aeronautics and Space Administration in a technical approach.
- Watch for Phase II follow-ons from the same firm/topic family — that conversion path is where budgets and transition pressure rise.
- Obligated amount $124,985. Cross-check similar awards in the same agency and technology tags for going-rate context.
- Topic code Z8 links this award to a solicitation family — search the same topic stem for incumbents and recompete timing.
- Amount
- $124,985
- Agency
- National Aeronautics and Space Administration
- Program / Phase
- SBIR · Phase I
- Topic
- Z8
- Solicitation
- SBIR_20_P1
- NAICS
- —
- Place of performance
- CA
- Period
- 2020-08-27 → 2021-03-01
Description
Flight Works is proposing to expand its micropump-fed propulsion technology to the development and demonstration of a low cost, compact, high performance lunar transfer stage designed for small launchers like Rocket Labrsquo;s Electron and Virgin Orbitrsquo;s Launcher One. With a total wet mass around 230 kg, the transfer stage is designed to provide high-thrust, high delta-V capabilities of over 3 km/s to one or more nanosat payloads weighing more than 30 kg. It will be to propel small spacecraft (CubeSat or nanosat) from Low Earth Orbit on to Trans Lunar Injection trajectories. The system can either stay attached to the small primary payload for long term mission operations, or deploy the latter at its destined lunar orbit.nbsp;This proposed effort builds on the extensive propulsion technology developed at Flight Works in the area of micro-pump-fed propulsion systems, combined with space system-level know-how of its principals, to provide a stage with unique benefits. These include compact, conformal low-pressure tanks/stage minimizing range safety operations and costs; high thrust for rapid, efficient transfer (compared with electric propulsion systems which have to be launched at higher orbits to avoid low altitude drag and which can require months to reach the targeted orbit); minimized size provided by a high performance propulsion system; and attitude control system during the delta-V maneuver which can ride along for cislunar operations.