Tungsten nuclear rocket, phase I, part 1 Final report
Tungsten water moderated nuclear rocket reactor experiments and analyses
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Tungsten water moderated nuclear rocket reactor experiments and analyses
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
Nonsteady flow conditions in subsonic section of Laval nozzle to investigate nonlinear transverse combustion instability in liquid propellant rocket motors
Design and development of rocket engine for spacecraft reaction control and maneuvering systems
Results from tests of rocket engine for spacecraft reaction control and maneuvering systems
Sound field measurements for shadowgraph hot model rocket exhaust flow experiments
Rocket sounding measurements of upper stratosphere and mesosphere
Design and evaluation of liquid hydrogen cooled rocket engine for determining minimum satisfactory coolant flow
Sounding rocket pressure,density, temperature, and wind measurements in upper stratosphere and mesosphere
Nike-Apache rocket ionospheric current measurements using rubidium-vapor magnetometer
Shadow photography of propellant spray behavior in liquid propellant rocket engine
Fluorine-liquid oxygen mixture and injector design effects on JP-4 jet fuel performance in rocket engines
Hydrogen-fluorine performance at low combustion chamber pressures in rockets with high area ratio exhaust nozzles
Performance tests of low pressure drop coaxial and shower-head injectors for gaseous hydrogen- liquid fluorine rocket chamber
Performance of liquid hydrogen-fluorine propellant combination in regeneratively cooled rocket engine
Transonic aerodynamic characteristics of two-stage fin-stabilized rocket launch vehicle in combination with winged spacecraft
Off-design performance levels for divergent- ejector-type rocket nozzles
Experimental performance of hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios