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Retractable Trunnion Pin MechanismThe X-38 is a technology demonstration project for the proposed International Space Station Crew Return Vehicle. The project consists of several atmospheric flight vehicles and an unmanned spacecraft. This paper will discuss the design, development, and testing of a Retractable Trunnion Pin Mechanism used to mount the spacecraft in the payload bay of the space shuttle orbiter for launch.
Document ID
20010071169
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Wayne Jermstad (Johnson Space Center Houston, United States)
Mark Landeck (Johnson Space Center Houston, United States)
Date Acquired
August 20, 2013
Publication Date
May 1, 2001
Publication Information
Publication: 35th Aerospace Mechanisms Symposium
Publisher: National Aeronautics and Space Administration
Volume: NASA/CP-2001-209626
Subject Category
Engineering (General)
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 35th Aerospace Mechanisms Symposium
Location: Sunnyvale, CA
Country: US
Start Date: May 9, 2001
End Date: May 11, 2001
Sponsors: Lockheed Martin (United States), Mechanisms Education Association, National Aeronautics and Space Administration
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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