Add to ORKGThe characteristics of a turbine pump for use with the nuclear engine for rocket vehicles are discussed. It was determined that the pump will be a two stage centrifugal pump with both stages having backswept impellers and an inducer upstream of the first stage impeller. The test program provided demonstration of the ability of the selected design to meet the imposed requirements
During the design of the NERVA turbopump, numerous computer programs were developed for the analyses...
Feasibility and operating characteristics of main tank of liquid hydrogen tank with fluorin
Modification of M- 1 liquid hydrogen turbopump for use in Phoebus nuclear reacto
The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located ...
The use of centrifugal pumps for rocket engines is described in terms of general requirements of ope...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
Small, high-performance LO2 and LH2 turbopump assembly configurations were selected, detail designs ...
A comprehensive analytical and experimental program was performed to evaluate the performance of a f...
A preliminary evaluation of pump performance was initiated to determine the efficiencies of an arbit...
A high pressure, liquid hydrogen turbopump was designed, fabricated, and tested to a maximum speed o...
Rotating and positive displacement pumps of various types were studied for pumping liquid fluorine f...
Prototype components fabrication and performance tests in development of hydrogen-oxygen auxiliary s...
Hubless pump inducer tested with shrouded centrifugal impeller, using water and liquid nitroge
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
The purpose of the study was to compare the performance of several configurations of hubless inducer...
During the design of the NERVA turbopump, numerous computer programs were developed for the analyses...
Feasibility and operating characteristics of main tank of liquid hydrogen tank with fluorin
Modification of M- 1 liquid hydrogen turbopump for use in Phoebus nuclear reacto
The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located ...
The use of centrifugal pumps for rocket engines is described in terms of general requirements of ope...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
Small, high-performance LO2 and LH2 turbopump assembly configurations were selected, detail designs ...
A comprehensive analytical and experimental program was performed to evaluate the performance of a f...
A preliminary evaluation of pump performance was initiated to determine the efficiencies of an arbit...
A high pressure, liquid hydrogen turbopump was designed, fabricated, and tested to a maximum speed o...
Rotating and positive displacement pumps of various types were studied for pumping liquid fluorine f...
Prototype components fabrication and performance tests in development of hydrogen-oxygen auxiliary s...
Hubless pump inducer tested with shrouded centrifugal impeller, using water and liquid nitroge
An abbreviated program was conducted to investigate igniter, injector, and thrust chamber technology...
The purpose of the study was to compare the performance of several configurations of hubless inducer...
During the design of the NERVA turbopump, numerous computer programs were developed for the analyses...
Feasibility and operating characteristics of main tank of liquid hydrogen tank with fluorin
Modification of M- 1 liquid hydrogen turbopump for use in Phoebus nuclear reacto