Flexible Transpiration Cooled Thermal Protection System for Inflatable Atmospheric Capture and Entry Systems

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$69,480.00
Award Year:
2006
Program:
SBIR
Phase:
Phase I
Contract:
NND06AA33C
Award Id:
77638
Agency Tracking Number:
054039
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
505 5th Avenue South, Suite 300, Seattle, WA, 98104
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
092968127
Principal Investigator:
DanaAndrews
Principal Investigator
(206) 438-0630
dandrews@andrews-space.com
Business Contact:
ChrisHoeft
Business Official
(206) 438-0602
choeft@andrews-space.com
Research Institute:
n/a
Abstract
Andrews Space, Inc. proposes an innovative transpiration cooled aerobrake TPS design that is thermally protective, structurally flexible, and lightweight. This innovative design will also meet launch volume constraints and satisfy terminal aerobraking requirements. The approach will focus on transpiration cooling of a flexible material and will consider ablative and insulative technologies as key features of the TPS design. The application of aerobraking to reduce velocity for planetary capture and landing has long been assumed for use on Mars missions and has been suggested for Earth reentry. The major hurdle to inflatable aerobrakes becoming reality is the development of a lightweight and structurally flexible Thermal Protection System (TPS). By combining well understood insulative and ablative TPS with an innovative flexible transpiration cooled TPS, a realizable inflatable aerobrake system can be developed.

* information listed above is at the time of submission.

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