Optimum thermal design through computer simulation of a space-vehicle structure in earth orbit.Optimal temperature control design using IBM 7094 digital computer program for thermal environment simulation of stabilized multisurfaced earth- orbiting spacecraft structure
Document ID
19670036701
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Feher, S. I.
Mccue, G. A.
Date Acquired
August 3, 2013
Publication Date
November 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
ASME PAPER 66-WA/HT-44Report Number: ASME PAPER 66-WA/HT-44