SBIR/STTR Research Award

High-Performance, Refuelable, “Green” Propulsion System for Multi-Object Removal/Retrieval System

Award identifier 9051d4d10b713784930a76161168d6fcb4e9e7ae685b5153a77924b54c617778Awarding agency National Aeronautics and Space Administration

Award amount

$3,999,526

Program and phase

SBIR · Phase II

Award year

2024

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Flight Works, Inc.
Proposal award date
2024-01-03
Contract end date
2026-01-02
UEI
CNN1EYNTU9Y7
Solicitation number
SEQ_23_P2S_C1
Topic code
Z8

Research abstract

Flight Works is proposing to address the issue of Active Debris Removal, Technical Need Area 2023-3, by modifying the high delta-V ldquo;greenrdquo; propulsion system of its Lunar Transfer Stage (a.k.a. Small Orbital Maneuvering Vehicle, S-OMV) for use in an active orbital debris removal/object retrieval system. This system relies on pump-fed ASCENT propulsion which drastically decreases inert mass fraction and allows operating the thrusters at their maximum Isp regardless of tank pressure. With the high density-Isp of ASCENT, the pump-fed system performance rivals with that of conventional bipropellant systems. With the bidirectional pump, the system can refuel itself from simple, low-cost tankers launched on demand or stored in space. ASCENT systems have yet to be designed for Rendezvous and Proximity Operations (RPO), however. Typically, the higher thruster duty cycle and preheat requirements needed with ASCENT (when compared with hydrazine) leads to larger impulse bit, hence coarser control, and increased power consumption. With the use of a pump, the control limitation can be circumvented, allowing the system to operate at different pressure points to best match thruster duty cycle for optimum system output depending on mission needs. Similarly, thrusters can be packaged for optimum thermal management to reduce preheat power. nbsp; As a result, the upgraded propulsion system has precise and efficient RPO capabilities. When integrated into a retrieval or disposal system, it is able to de-orbit multiple 100 kg-sized objects, or up to a single 3,000 kg object initially orbiting at 500 km, or 1,200 kg at 1,000 km, before re-boosting itself into orbit for refueling. Refueling can be accomplished at low cost with Flight Worksrsquo; Medium-OMV-based simple tankers, and thus increase the total disposal capacity to over ten metric tons. nbsp; As a first step toward commercial operations, Flight Works plans to supply the system to a private firm for retrieval of a historical space artifact.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

22 SBIR/STTR records share this UEI (2008–2025). Reported award amounts total $16,573,476. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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