SBIR/STTR Research Award

High-Performance, High Thrust, “Green” Orbital Maneuvering Vehicle for Lunar and Deep Space Missions

Award identifier 2ce45c5ad98c200aef8f18630fc0656e53047a8af8e5fb629d40dab952f2aacdAwarding agency National Aeronautics and Space Administration

Award amount

$4,999,071

Program and phase

SBIR · Phase II

Award year

2022

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Flight Works, Inc.
Proposal award date
2022-09-29
Contract end date
2024-09-28
UEI
CNN1EYNTU9Y7
Solicitation number
SEQ_22_P2S_C1
Topic code
S3

Research abstract

Flight Works is proposing to continue the development and demonstration of a high-performance Orbital Maneuvering Vehicle (OMV) which enables dedicated missions to cislunar and deep space (such as Mars rendezvous) with small launchers like Virgin Orbitrsquo;s Launcher One and ABLrsquo;s RS-1. It features a full set of avionics flight-proven in LEO. These are to be modified for deep space missions with radiation tolerant components, additional redundancy, and upgraded communication system. The high performance is enabled by Flight Worksrsquo; micropump-fed propulsion technology combined with the high density-specific impulse (Isp) provided by the green monopropellant ASCENT, with long life thrusters based on the technology developed for the NASA Lunar Flashlight CubeSat. For deep space missions, the green propellant can be stored cold to minimize heating power and a low-power pumped loop can be used to slightly warm the propellant prior to use. The result is a simple, versatile, cost-effective OMV with performance capabilities similar to that of a traditional bipropellant pressure-fed stage and which can be configured for dedicated cislunar and Mars missions. The OMV has approximately twice the capability of Rocket Labrsquo; upgraded Photon to be used on NASA CAPSTONE and ten times that of Momentus Vigoride.nbsp;The system is scalable by decreasing or increasing tank size. Also, the use of a green propellant and low-pressure tanks minimizes range safety operations and costs. The medium thrust allows for rapid, efficient transfer compared with electric propulsion systems which have to be launched at higher orbits to avoid low altitude drag and require months to reach the targeted orbit while exposing the system to the damaging radiation of the Van Allen belts. Finally, the pump in the propulsion system enables an extension to servicing missions (with the addition of proximity operations and docking features), with the OMV acting either as client or servicer.

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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