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Shuttle detached spacecraft

Author: Roger E Jacobs; U.S. Air Force Geophysics Laboratory. Aerospace Instrumentation Division.
Publisher: Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory Air Force Systems Command, United States Air Force, 1983.
Series: AFGL-TR, 84-0054.; Instrumentation papers, no. 323.
Edition/Format:   Print book : National government publication : EnglishView all editions and formats
Summary:
This report reports the results of a year-long in-house effort to investigate the potential utility and economic feasibility of developing a standard shuttle experiment support system to satisfy Air Force Geophysics Laboratory (AFGL) scientific requirements. It is shown that a shuttle detachable spacecraft capable of operating away from the orbiter environment, as well as attached in the cargo bay, maximizes its  Read more...
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Details

Additional Physical Format: Online version:
Jacobs, Roger E.
Shuttle detached spacecraft
(OCoLC)1045074546
Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Roger E Jacobs; U.S. Air Force Geophysics Laboratory. Aerospace Instrumentation Division.
OCLC Number: 11007755
Notes: Cover title.
"30 December 1983."
"Project 7659."
Aerospace Instrumentation Division Project 7659.
Distributed to depository libraries in microfiche.
Description: 23 pages : illustrations ; 28 cm.
Series Title: AFGL-TR, 84-0054.; Instrumentation papers, no. 323.
Other Titles: Technical Report Archive & Image Library (TRAIL)
Responsibility: Roger E. Jacobs.

Abstract:

This report reports the results of a year-long in-house effort to investigate the potential utility and economic feasibility of developing a standard shuttle experiment support system to satisfy Air Force Geophysics Laboratory (AFGL) scientific requirements. It is shown that a shuttle detachable spacecraft capable of operating away from the orbiter environment, as well as attached in the cargo bay, maximizes its usefulness as an experiment support platform. A philosophy of minimum shuttle interface and efficient utilization of cargo bay volume is incorporated in an effort to reduce costs and provide greater flexibility for launch opportunities. (Author).

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