Grant For Research 80NSSC18K0032

Award Date 11/17/17
Potential Completion Date 12/31/18
Potential Value $286K
Awardee
Msnw LLC
Ultimate Awardee
Not listed
NAICS Category
Not listed
Federal Contract Vehicle
Set-Aside Type
No Set-Aside Used
Extent Competed
Full and Open Competition
Major Defense Program
Not listed
Pricing Type
Other
Place of Performance
Redmond, WA 98052, USA
Solicitation Procedures
Basic Research
Number Of Offers Received
Not listed
Legislative Mandate
Not listed
National Interest Action
Not listed
Research Type
Not listed
Primary Consortia Member
Not listed
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The proposed technology aims to utilize a simple dipole magnetic field containing a magnetized plasma to interact with a planetary atmosphere and produce significant drag forces, enabling aerocapture and reducing the need for large, heavy, and risky aeroshells or inflatable ballutes. Phase I design studies showed the potential to enable aerocapture of large payouts at Mars and Neptune without the need for dedicated thermal protection systems. The Phase II effort will further validate the technology through detailed mission studies, plasma-neutral interaction testing, and development of a 3D aerocapture orbital dynamics model.

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