SBIR/STTR Research Award

ISS Launched Cubesat Demonstration of Variable-Drag Magnetoshell Aerocapture

Award identifier 1d7cd9684d81724f73ccf328ca423ded9cccc5d96a152007f003e030420db2b2Awarding agency National Aeronautics and Space Administration

Award amount

$124,999

Program and phase

SBIR · Phase I

Award year

2014

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
MSNW LLC
Proposal award date
2014-06-20
Contract end date
2014-12-19
UEI
ZUJKEA8YLMC6
Solicitation number
Not reported
Topic code
H20.02

Research abstract

Aerobraking and aerocapture have been shown to be mission enabling for deep space orbiters and manned missions, and yield dramatic cost and mass savings for near earth missions. However, high dynamic pressure aerocapture is high risk and requires large, complex, and heavy deflector shells. Magnetoshell Aerocapture (MAC) is a revolutionary technology that has been developed by NASA and MSNW that can enable low-cost, low-risk aerocapture for a range of Earth and deep space missions. The Magnetoshell deploys a simple dipole magnetic field containing a magnetized plasma. Interaction of neutral particles in the atmosphere with this magnetized plasma produces the desired drag for braking, acting in effect like a plasma parachute. With the aeroshell now being composed of a massless magnetic field, the scale of the shell can be as large as 100 meters with only a gram of plasma and a simple copper magnet. Drag can be dynamically controlled in response to atmospheric conditions, enabling very aggressive aerocapture maneuvers. By providing pulsed power, the thermal and power processing requirements can be kept within the scope of conventional technologies. In a Phase I NIAC program a 1.6 meter diameter Magnetoshell was demonstrated and increased the drag force of a supersonic flowing neutral jet by 1000X. A wide range of mission studies showed that MAC can enable a Neptune orbiter mission, reduce the cost of a manned Martian mission by $2B, and provide the low-cost drag system for Earth return missions. In the following proposal a three year ISS-launched CubeSat demonstration mission paves the way for full scale operation missions. In Phase I a complete system design will be completed and several of the primary technology risks will be mitigated. When demonstrated, Magnetoshell Aerocapture will dramatically reduce cost and risk for applications ranging from nanosatellites, deep space Flagship science missions, and commercial applications such as reusable tankers.

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

National Aeronautics and Space Administration

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