SBIR/STTR Research Award

FRC Multi-Mode Thruster Validation Demonstration

Award identifier 3196e3690c43546b4c3afaf02cb8e3127abac35d077fa54e35b06fbb8a1e553bAwarding agency Department of Defense · Air Force

Award amount

$748,823

Program and phase

SBIR · Phase II

Award year

2013

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
MSNW LLC
Proposal award date
2013-02-22
Contract end date
2015-06-01
UEI
ZUJKEA8YLMC6
Solicitation number
2011.2
Topic code
AF112-177

Research abstract

ABSTRACT: Modern military space systems use high specific impulse (Isp) propulsion systems to provide efficient station keeping and large delta-V orbital maneuvers. A multi-mode propulsion system utilizes a single propellant such as AF-M315E to provide high thrust as well as a 1000-4000 s Isp. By utilizing the same propellant in multiple thrusters an entire new range of mission operations are possible. The same spacecraft design and propulsion subsystem can be used over a wide range of mission operations from orbital plane changes to station keeping. Perhaps most importantly is the ability to provide on command dynamic mission changes for avoidance, for rendezvous, or precision observation all without a preordained mission set. The proposed development program will demonstrate and characterize the EMPT-MM, a 1.6 - 5 kW FRC thruster capable of efficient operation of Hydrazine, Xenon, and AF-M315E. In Phase I a direct liquid injection and pre-ionization system was demonstrated. In Phase II, this injector will be combined with a 1 kW thruster that will be demonstrated at MSNW and AFRL facilities running in steady operation on full AF-M315E propellant. At the conclusion of Phase II, a high-efficiency, wide specific impulse range multi-mode thruster will be developed, demonstrated, and delivered to AFRL. BENEFIT: Modern lightweight solar panel technology, such as the DARPA FAST program, has created a unique need for lightweight, efficient, and highly variable power Electric Propulsion.T the ability to use complex propellants such as Air, AF-M315E, or Hydrazine would allow a dramatic shift in the capabilities of DOD spacecraft. An EP system operating at high specific impulse on monopropellants could be retasked indefinitely between station keeping and rapid orbital maneuvers using a single propellant. Additionally, the ability to use ambient atmospheric gases would enable highly-eccentric orbits that use ambient Air for orbit raising and drag reduction for very low orbits. The Multi-Mode FRC thruster has definite payoffs for long-term military missions. This technology has direct applicability to missions involving Space Situational Awareness, orbit raising tugs, Dynamic and operationally responsive space, as well as all high delta-V missions such as plane changes. A Multi-Mode electric propulsion system capable of operation with any complex, liquid propellant has applications for DOD high-power EP, DOD rapid response propulsion, and NASA science missions.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

26 SBIR/STTR records share this UEI (1999–2017). Reported award amounts total $8,094,788. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

Department of Defense

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