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Space Shuttle booster recovery planning.At the initiation of the Space Shuttle Program, recoverable solid rocket boosters were base-lined, with an estimated savings of 30 per cent over expendable solid rockets. Present studies indicate that the solid rocket boosters in the 142-inch diameter range can be recovered using state-of-the-art recovery systems. Marshall Space Flight Center is conducting extensive studies to establish the most cost effective recovery system for the present Shuttle boosters. Model drop testing, in various facilities, and structural load testing are being conducted with model sizes ranging from 6 inches to 120 inches in diameter.
Document ID
19730046625
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Godfrey, R. E.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1973
Subject Category
Aircraft
Report/Patent Number
AIAA PAPER 73-441
Meeting Information
Meeting: Aerodynamic Deceleration Systems Conference
Location: Palm Springs, CA
Start Date: May 21, 1973
End Date: May 23, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A31427
Distribution Limits
Public
Copyright
Other

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