The thermal design analysis and flight data evaluation of JACEE-13

1996 ◽  
Author(s):  
Steve Spencer ◽  
T. Parnell
Keyword(s):  
Design Analysis ◽  
Thermal Design ◽  
Data Evaluation ◽  
Flight Data

An Insight into the Features of the OAO-C Thermal Design

1973 ◽  
Vol 95 (4) ◽  
pp. 1039-1047 ◽  
Author(s):  
H. Fine ◽  
J. Quadrini ◽  
S. Ollendorf
Keyword(s):  
Thermal Control ◽  
Astronomical Observatory ◽  
Thermal Design ◽  
Test Bed ◽  
Large Space ◽  
Flight Data ◽  
The Earth ◽  
Ground Test ◽  
Earth Observation Satellite ◽  
Insight Into

The Orbiting Astronomical Observatory (OAO)-C was successfully launched into 400-nautical mile circular orbit on August 21, 1972. For this spacecraft, a unique sensitivity approach to the thermal design was developed which resulted in a predictal design—the merits of which should be considered for application on future spacecra. The OAO-C is also serving as a test bed for the evaluation of thermal control hardware. To provide flight data for space program applications, experiments for a new coating and four different heat pipe designs are on this spacecraft. The data derived from OAO-C will be extremely valuable for such future programs as the Large Space Telescope (LST) and the Earth Observation Satellite (EOS). This paper will describe the detailed of the sensitivity design approach and thermal control hardware. For all aspects discussed, a comparison of pertinent analysis, ground test data, and flight data [1] will be given.

Thermal design, analysis, and experimental verification for a DIII-D cryogenic pump

1991 ◽  
Vol 18 ◽  
pp. 223-226 ◽  
Author(s):  
C.B. Baxi ◽  
P. Anderson ◽  
A. Langhorn ◽  
K. Schaubel ◽  
J. Smith
Keyword(s):  
Experimental Verification ◽  
Design Analysis ◽  
Thermal Design ◽  
Cryogenic Pump

Thermal Design Analysis Supporting a Loss-of-Coolant-Accident Experiment at TREAT

2020 ◽  
Author(s):  
C. Folsom ◽  
C. Jensen ◽  
N. Woolstenhulme ◽  
R. Armstrong
Keyword(s):  
Design Analysis ◽  
Thermal Design ◽  
Loss Of Coolant Accident ◽  
Loss Of Coolant

The Cassini INCA sensor - Thermal design, analysis and test

1996 ◽  
Author(s):  
Edward Lin ◽  
Ronald Reeve ◽  
Glenn Tsuyuki ◽  
James Stultz
Keyword(s):  
Design Analysis ◽  
Thermal Design
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