NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Thermal environments for Space Shuttle payloadsThe thermal environment of the Space Shuttle payload bay during the on-orbit phase of the STS flights is presented. The STS Thermal Flight Instrumentation System and various substructures of the Orbiter and the payload are described, as well as the various on-orbit attitudes encountered in the STS flights (the tail to sun, nose to sun, payload bay to sun, etc.). Included are the temperature profiles obtained during the on-orbit STS 1-5 flights (with the payload bay door open), recorded in various substructures of the Orbiter's midsection at different flight attitudes, as well as schematic illustrations of the Space Shuttle system, a typical mission profile, and the Orbiter's substructures.
Document ID
19860029642
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fu, J. H.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Graves, G. R.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 85-6058
Accession Number
86A14380
Distribution Limits
Public
Copyright
Other

Available Downloads

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