Nucleonic Propellant Gaging and Utilization Systems for Space Vehicles

640487

01/01/1964

Event
SAE World Congress & Exhibition
Authors Abstract
Content
A typical nucleonic propellant gaging and utilization system for space vehicles is described, together with a detailed discussion of the individual components. Photographs of prototype installations and test results of these configurations are presented to substantiate the theoretical analyses for signal propagation and radiation pattern mapping including measurements under zero gravity conditions. The results are concluded as verifying the nucleonic measurement system capability for providing an accurate, highly reliable approach to maximum cost effectiveness of propellant gaging and utilization system design.
Meta TagsDetails
DOI
https://doi.org/10.4271/640487
Pages
7
Citation
Wright, D., "Nucleonic Propellant Gaging and Utilization Systems for Space Vehicles," SAE Technical Paper 640487, 1964, https://doi.org/10.4271/640487.
Additional Details
Publisher
Published
Jan 1, 1964
Product Code
640487
Content Type
Technical Paper
Language
English