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COLD-SAT - A technology satellite for cryogenic experimentationNASA-Lewis (LeRC) is involved in the development and validation of analytical models which describe the fluid dynamic and thermodynamic processes associated with the storage, acquisition and transfer of subcritical cryogenic fluids in low gravity. Four concurrent studies, including one in-house at LeRC, are underway to determine the feasibility of performing model validation experiments aboard a free-flying spacecraft (S/C) called Cryogenic On-Orbit Liquid Depot-Storage, Acquisition and Transfer (COLD-SAT), using liquid hydrogen as the cryogen. The technology requirements for the experiments are described along with the initial LeRC concepts for the S/C and an experiment subsystem comprising of cryogenic tankage (a supply dewar and three receiver tanks), gas pressurization bottles (both helium and autogenous hydrogen), their associated plumbing, and instrumentation for data collection. Experiments were categorized into enabling/high priority Class 1 technologies and component/system Class 2 demonstrations. As initially envisioned by LeRC, COLD-SAT would have had a 1997 launch aboard a Delta-2 for a 6 month active lifetime in a 925 km orbit with a pseudo-inertial attitude.
Document ID
19920030801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Arif, H.
(NASA Lewis Research Center Cleveland, OH, United States)
Kroeger, E. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: 1989 Cryogenic Engineering Conference
Location: Los Angeles, CA
Country: United States
Start Date: July 24, 1989
End Date: July 28, 1989
Accession Number
92A13425
Distribution Limits
Public
Copyright
Other

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