Add to ORKGActivation and initial test operations of thrust chamber facility for NASA M-1 rocket engin
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
A high pressure, liquid hydrogen turbopump was designed, fabricated, and tested to a maximum speed o...
Mechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engin
Hydrostatic life-off seal zero leakage and static sealing and rubbing tests for use in liquid hydrog...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and...
Thermal conditioning problems of liquid hydrogen turbopumps to enhance mixed-phase operation and to ...
Liquid hydrogen film cooled pressure transducer for flush mounting in rocket combustion chambe
The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located ...
Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Shaftwhirling critical speeds and bearing loads for model I and model II fuel turbopump
Instrumentation and data acquisition system for development testing of liquid hydrogen/liquid oxygen...
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...
A high pressure, liquid hydrogen turbopump was designed, fabricated, and tested to a maximum speed o...
Mechanical design of two-stage impulse turbine for liquid hydrogen turbopump of M-1 engin
Hydrostatic life-off seal zero leakage and static sealing and rubbing tests for use in liquid hydrog...
Engineering criteria for thermodynamic improvenent of liquid hydrogen turbopumps for rocket engine
Hydrogen turbopump cycles for obtaining high engine inlet pressures in advanced nuclear rockets, and...
Thermal conditioning problems of liquid hydrogen turbopumps to enhance mixed-phase operation and to ...
Liquid hydrogen film cooled pressure transducer for flush mounting in rocket combustion chambe
The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located ...
Analysis, design, and demonstration of high performance injectors for liquid fluorine- gaseous hydro...
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrus...
Shaftwhirling critical speeds and bearing loads for model I and model II fuel turbopump
Instrumentation and data acquisition system for development testing of liquid hydrogen/liquid oxygen...
Activation and initial test operations of thrust chamber facility for NASA M-1 rocket engin
Design and environmental testing of thermal conditioning unit for liquid hydrogen propellant tan
Analysis of reactor heated Brayton cycle space power plants - Models of gas and liquid-metal reactor...