NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design and test of a modified passive orbital disconnect strut (PODS-IV)The design and testing of a modification to the Passive Orbital Disconnect Struts (PODS) III system (designed to reduce support conductance and superfluid-helium-tank dewar weights), PODS IV, are discussed. The PODS IV design was found to achieve a nominal increase of 630-812 percent in side-load resistance over the PODS-III design, with a predicted 15-percent increase in thermal conductance. It is noted that the increase in side-load resistance largely removes the limitation on length of the orbit tube inherent in the PODS III design. The higher resistance of the longer orbit tube results in lower total conductance for the PODS-IV design.
Document ID
19880065999
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spradley, Iran E.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Parmley, Richard T.
(Lockheed Missiles and Space Co., Inc. Research and Development Div., Palo Alto, CA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Advances in cryogenic engineering.
Location: Saint Charles, IL
Country: United States
Start Date: June 14, 1987
End Date: June 18, 1987
Accession Number
88A53226
Funding Number(s)
CONTRACT_GRANT: NAS2-11946
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available