Experimental auxiliary rocket engine, part II Final report
Results from tests of rocket engine for spacecraft reaction control and maneuvering systems
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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
Design and performance characteristics of variable dynamic force vector rocket test apparatus
Nitrogen tetroxide and blend of hydrazine and unsymmetrical dimethyl hydrazine evaluated in rocket engines with large area ratio nozzles - Apollo project
Altitude compensation and thrust augmentation studied in mixing effects of supersonic flows of rocket engine
Design of small animal payload and integration with sounding rocket for space flight research