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A detached experiment carrier aids adaptation of experiments from sounding rockets to Space ShuttleThe detached experiment carrier (DEC) system aids the adaptation of small, low-weight experiments to Space Shuttle missions. The carrier system consists of the detached experiment carrier (free-flyer), a command station at the Orbiter aft station, and a flight support station in the Orbiter payload bay. The carrier is a compact vehicle that is radio controlled by the Shuttle crew. It uses control television, command, and cold gas propulsion systems to deploy experiments from and later rendezvous with the Orbiter. The carrier propulsion system also maintains the attitude control required during experiment execution. Results of engineering investigation, analysis, component design and development, and testing indicate that the DEC system concept is practical. Results of preliminary engineering investigations, including maneuvering system handling qualities and television/telemetry display formats, indicate that the concept of flying the DEC 'out of' and 'into' the Orbiter payload bay is both safe and practical for small, compact free-flyer deployment and retrieval. This paper describes the carrier system, its operations, and potential applications.
Document ID
19790041741
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Ritz, W. F.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Whitsett, C. E.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 79-0484
Report Number: AIAA PAPER 79-0484
Meeting Information
Meeting: Sounding Rocket Technology Conference
Location: Houston, TX
Start Date: March 7, 1979
End Date: March 9, 1979
Accession Number
79A25754
Distribution Limits
Public
Copyright
Other

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