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Dedicated Deployable Aerobraking StructureA dedicated deployable aerobraking structure concept was developed that significantly increases the effective area of a spacecraft during aerobraking by up to a factor of 5 or more (depending on spacecraft size) without substantially increasing total spacecraft mass. Increasing the effective aerobraking area of a spacecraft (without significantly increasing spacecraft mass) results in a corresponding reduction in the time required for aerobraking. For example, if the effective area of a spacecraft is doubled, the time required for aerobraking is roughly reduced to half the previous value. The dedicated deployable aerobraking structure thus enables significantly shorter aerobraking phases, which results in reduced mission cost, risk, and allows science operations to begin earlier in the mission.
Document ID
20100028884
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other - NASA Tech Brief
Authors
Giersch, Louis R.
(California Inst. of Tech. Pasadena, CA, United States)
Knarr, Kevin
(California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
August 1, 2010
Publication Information
Publication: NASA Tech Briefs, August 2010
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NPO-47227
Distribution Limits
Public
Copyright
Public Use Permitted.
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