DocumentCode :
1231069
Title :
Saturn S-IV Cryogenic Weigh System Part II: Weigh Operations
Author :
Matsumoto, G.A.
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 :
152
Lastpage :
159
Abstract :
Two basic methods for mass determination are: (1) direct measurement, (2) volume and density determination. Both methods or variations have been used to determine space vehicle propellant mass with varying degrees of success. Stringent propellant loading accuracy requirements of ??0.5 percent for the Saturn S-IV Stage have led to the development of a Cryogenic Calibration Weigh System. The method employs accurate electronic force transducers and measuring systems as the standard and experimental weighings have verified achievement of better than the required accuracy.
Keywords :
Calibration; Cryogenics; Density measurement; Force measurement; Measurement standards; Propulsion; Saturn; Space vehicles; Transducers; Volume measurement;
fLanguage :
English
Journal_Title :
Aerospace, IEEE Transactions on
Publisher :
ieee
ISSN :
0536-1516
Type :
jour
DOI :
10.1109/TA.1965.4319796
Filename :
4319796
Link To Document :
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