Nucleonic Cryogenic Propellant Gaging System
Nucleonic Cryogenic Propellant Gaging System
- New search for: J. R. Webster
- New search for: J. R. Webster
The objectives of this program were to design, fabricate and ground test a prototype propellant gaging system capable of operating with high energy, cryogenic liquid fluorine (LF2) and liquid hydrogen (LH2) propulsion systems for future upper-stage booster space maneuvering missions. This report details the analysis of the nucleonic methods considered for cryogenic propellant gaging and delineates the results of feasibility study of such techniques. (Author)
Document information
Nucleonic Cryogenic Propellant Gaging System
1969
135 pages
Report
No indication
English
Rocket Propellants , Laboratory & Test Facility Design & Operation , Nuclear Instrumentation , Cryogenic propellants , Fuel gages , Propellant tanks , Nuclear radiation , Space propulsion , Fuel consumption , Gamma rays , Attenuation , Scattering , Feasibility studies , Radioactive isotopes , Radiation monitors , Photomultiplier tubes , Scintillation counters , Detectors , Packaging , Design , Manufacturing , Structural properties , Thermal analysis , Reliability
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