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Mars lander thermal control system parametric studies.Mars lander thermal control system design parameters including environment, power duty cycle and lander size and weight
Document ID
19690055285
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Morey, T. F.
Tracey, T. R.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AIAA PAPER 69-610
Report Number: AIAA PAPER 69-610
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, THERMOPHYSICS CONFERENCE
Location: SAN FRANCISCO, CALIF.
Start Date: June 16, 1969
End Date: June 18, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A33274
Funding Number(s)
CONTRACT_GRANT: NAS1-7590
CONTRACT_GRANT: NAS1-7976
Distribution Limits
Public
Copyright
Other

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