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Payload deployment method and systemA method and apparatus for deploying the payload of space shuttle or the like is described. It is referred to as the Stabilized Payload Deployment System (SPDS). The payload is rotated about an axis outside of the payload but approximately longitudinally with the cargo bay of the shuttle craft. The payload may thus be rotated through ninety degrees. In this case, that is, in its rotated position, the payload may or may not have a small portion located within the cargo bay. Alternatively, the payload may be located completely outside of the bay. According to the apparatus two separable hinge-like devices connect at one longitudinal side or edge of the payload to respective ones of the payload trunnions at different longitudinally spaced locations along the length of the payload. Separation of the payload from the cargo bay is made by unlatching a latch and by the use of a repulsion spring at the position of each hinge-like device. Two four-link mechanisms allow movement between payload and bay. Such accommodative movement is required especially during launch when considerable vibration is encountered.
Document ID
19880015276
Acquisition Source
Legacy CDMS
Document Type
Other - Patent Application
Authors
Barnett, Clifford J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Greenwood, John E.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Holman, Earl V.
(Rockwell International Corp. Houston, Tex., United States)
Date Acquired
September 5, 2013
Publication Date
April 15, 1988
Subject Category
Space Transportation
Report/Patent Number
NAS 1.71:MSC-21330-1
Accession Number
88N24660
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-MSC-21330-1
Patent Application
US-PATENT-APPL-SN-182000
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