DocumentCode :
1231078
Title :
Saturn S-IVB Cryogenic Weigh System Part III: Environmental Control
Author :
Ross, Edwin C.
Author_Institution :
Missile and Space Systems Division Douglas Aircraft Company, Inc. Huntington Beach, Calif.
Issue :
2
fYear :
1965
fDate :
6/1/1965 12:00:00 AM
Firstpage :
160
Lastpage :
166
Abstract :
In order to provide stage pre-launch thermal environment and to prevent frost formation on the exterior tank surfaces, it was necessary to provide a heated, gaseous nitrogen atmosphere around the stage during cryogenic calibration. Frost formation is undersirable since it would add to the stage tare weight by an unknown amount. Nitrogen conforming to military dryness and cleanliness specifications was chosen for use in contact with the stage skin because of its low moisture content, its inertness with hydrogen or oxygen, its availability, and cost. This paper presents the design concepts of the S-IV and S-IVB stage systems, an appraisal of the S-IV design, and the design changes in the S-IV system as a result of the S-IV experience.
Keywords :
Atmosphere; Calibration; Control systems; Costs; Cryogenics; Hydrogen; Moisture; Nitrogen; Saturn; Skin;
fLanguage :
English
Journal_Title :
Aerospace, IEEE Transactions on
Publisher :
ieee
ISSN :
0536-1516
Type :
jour
DOI :
10.1109/TA.1965.4319797
Filename :
4319797
Link To Document :
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