Add to ORKGData tables for optimal thermal protection of liquid hydrogen storage in nuclear interplanetary spacecraf
Computer simulation studies of liquid hydrogen fill and vent systems for the space shuttle are studi...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
A computer programmer's manual for a digital computer which will permit rapid and accurate parametri...
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal prote...
Preliminary parametric analyses on earth orbital storage of liquid hydrogen propellant for manned Ma...
Thermal protection systems for cryogenic fuels - liquid hydrogen for space mission
The analysis on the feasibility for using metal hydrides in the thermal protection system of cryogen...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
Tasks accomplished during the HTTA Program study period included: (1) performance of a literature re...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and...
Size and shield weight requirements calculated for fast-spectrum, liquid-metal cooled nuclear reacto...
Viewgraphs on computational fluid dynamics (CFD) for nuclear thermal propulsion are presented. Topic...
Thermal analysis of space hold performance of multilayer insulation on upper half of unshrouded liqu...
A summarization and categorization is presented of the pertinent literature associated with cryogeni...
Computer simulation studies of liquid hydrogen fill and vent systems for the space shuttle are studi...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
A computer programmer's manual for a digital computer which will permit rapid and accurate parametri...
Technical analyses and computer programs in support of optimization of liquid hydrogen thermal prote...
Preliminary parametric analyses on earth orbital storage of liquid hydrogen propellant for manned Ma...
Thermal protection systems for cryogenic fuels - liquid hydrogen for space mission
The analysis on the feasibility for using metal hydrides in the thermal protection system of cryogen...
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
Tasks accomplished during the HTTA Program study period included: (1) performance of a literature re...
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and...
Size and shield weight requirements calculated for fast-spectrum, liquid-metal cooled nuclear reacto...
Viewgraphs on computational fluid dynamics (CFD) for nuclear thermal propulsion are presented. Topic...
Thermal analysis of space hold performance of multilayer insulation on upper half of unshrouded liqu...
A summarization and categorization is presented of the pertinent literature associated with cryogeni...
Computer simulation studies of liquid hydrogen fill and vent systems for the space shuttle are studi...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
A computer programmer's manual for a digital computer which will permit rapid and accurate parametri...