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Entry, Descent and Landing Using BallutesThe In Space Propulsion Program is funding a team lead by Kevin Miller at Ball Aerospace. This team of Industry, NASA, and Academic researchers is actively pursuing ballute technology development, with very promising results. The focus of that study has been to maximize the payload that is put into orbit (around Titan, Neptune, and Mars). So far the mass associated with the ballute has been minimized, because it was being thrown away. If an instrument package is attached to the Ballute, it will eventually land on the surface. Thus, the Ballute can do double duty: Aerocapture the Orbiter and Soft-land a set of instruments on the surface.
Document ID
20070014658
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Lyons, Daniel t.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
McRonald, Angus
(Global Aerospace Corp. CA, United States)
Date Acquired
August 23, 2013
Publication Date
April 1, 2005
Publication Information
Publication: 2nd International Planetary Probe Workshop
Subject Category
Space Sciences (General)
Distribution Limits
Public
Copyright
Public Use Permitted.
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