This paper describes the application of capacitive propellant gaging techniques to the aerospace enivronment. The propellant utilization and gaging system developed for Apollo is presented. In addition, some problems peculiar to aerospace and the solutions of these problems are discussed.
Propellant Gaging and Utilization for the Apollo Spacecraft
Sae Technical Papers
SAE World Congress & Exhibition ; 1964
1964-01-01
Conference paper
English
Propellant gaging and utilization for apollo spacecraft
Engineering Index Backfile | 1964
|Nucleonic propellant gaging and utilization systems for space vehicles
Engineering Index Backfile | 1964
|NTIS | 1987
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