NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The Skylab ParasolAn alternate thermal protection system for the Skylab space station cluster was deemed necessary shortly after launch when severe damage occured to the orbital workshop as it passed through the period of maximum dynamic pressure. Data indicated that the combination micrometeoroid and thermal shield on the sun facing side of the vehicle had been destroyed. The simultaneous design, fabrication, and test of the Skylab Parasol System which was completed in 6 days of around-the-clock effort is described. The Skylab Parasol design was selected as the primary sunshade device based on simplicity of design, ability to fabricate quickly, and early demonstration of a working prototype which featured semiautomatic deployment from within the workshop under shirt sleeve environment conditions.
Document ID
19760012092
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kinzler, J. A.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1975
Publication Information
Publication: 9th Aerospace Mech. Symp.
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N19180
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available