Analytical investigation of three turbopump feed systems suitable for high-pressure hydrogen-oxygen rocket-engine applications
Turbopump feed systems for high pressure hydrogen- oxygen rocket engines
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Turbopump feed systems for high pressure hydrogen- oxygen rocket engines
Rhodium, rhenium, and tungsten as cesium-ionizer materials in surface ionization engines
Solutions for angular motion equations of rotating space station by approximation method using small angle theory and exact computer method
Driving and controlling helicopter rotor by deflectable jet flap - theoretical study of jet-flat rotor characteristics
Effects of radiation in vacuum on mechanical properties of rigid plastics
Work function characteristics of metals immersed in cesium vapor - surface interaction
Thrust vector orientation during pilot controlled lunar landing with aid of visual references
Peripheral wall conduction effect on laminar forced convection in rectangular channels
Ignition and propagation of turbulent flame front in jet flow investigated for combustible hydrogen- air mixture
Pressurized liquid hydrogen tank outflow analysis
Peripheral wall conduction effect on laminar forced convection in rectangular channels
Heat transfer to nitrogen from baths of distilled water and ethyl alcohol during bubble formation from submerged orifice
Predicted and observed calorimetric exhaust efficiencies of capacitor powered coaxial plasma guns
Control of spacecraft internal temperature using movable shutters reflecting diffusely
Jacchia static diffusion models of upper atmosphere densities with empirical temperature profile
Thermal or helium lift pumping systems on space vehicle propellant feed systems preventing geysering and engine prestart propellant conditioning
Solutions to hydrogen-oxygen reaction ignition kinetics
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