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Advanced space recovery systemsThe design evolution of a space recovery system designed by a NASA-contracted study is described, with particular attention given to the design of a recovery system for a propulsion/avionics module (P/AM), which weighs 60,000 lb at the recovery initiation and achieves subsonic terminal descent at or above 50,000 ft msl. The components of the recovery system concept are described together with the operational sequences of the recovery. The recovery system concept offers low cost, low weight, good performance, a potential for pinpoint landing, and an operational flexibility.
Document ID
19890059429
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wailes, William K.
(Pioneer Aerospace Corp. Melbourne, FL, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 89-2399
Accession Number
89A46800
Funding Number(s)
CONTRACT_GRANT: NAS8-36631
Distribution Limits
Public
Copyright
Other

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