"Saturn S-IV cryogenic weigh system. Part II : weigh operations."
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 k0.5 percent for the...
Main Author: | Matsumoto, G. A. |
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Format: | Electronic |
Published: |
University of Alabama in Huntsville Archives
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Subjects: | |
Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10582 |
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