Design study of heat sterilizable solid rocket motors for space application, volume I Final report, Oct. 19, 1965 - Jan. 9, 1966
Design and analysis of heat sterilizable solid propellant rocket motors
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Design and analysis of heat sterilizable solid propellant rocket motors
Photographic study to obtain injection and combustion patterns of F-1 rocket engine injector elements
Temperature and density measurements in base region flow field of clustered rocket engine model using electron beam technique
Critical experiments and nuclear analyses of tungsten water moderated nuclear rocket reactor
Cratering effect of descending rocket exhaust expected from soft earth landing
Early U.S.S.R. multistage rocket developments based on Tsiolkovskii concepts
Solid state device for controlling temperature of optical birefringence filter for sounding rockets
Field effect electrometer amplifier for measuring ionospheric electric fields by sounding rockets and satellites
Test firing of 100-lb thrust ablatively cooled rocket chambers
Development of fast response temperature gauge for rocket vehicle plumbing systems
Solid propellant rocket engine performance computer programs using group transformation method
Transpiration and film cooling of liquid rocket nozzles
Design modifications, proof test, and delivery program of igniters for Recruit rocket engines
Increased performance of rocket engine using fluorine-oxygen mixture with RP-1 fuel
One-dimensional analysis of variable area mixing and combustion process in supersonic ramjet and rocket-ramjet hybrid engines
Wall temperature and heat transfer patterns in liquid-propellant rocket thrust chamber coolant channels
Evaluation of erosion resistant materials for throat inserts of ablative nozzle sections in storable propellant rocket engine
Topping and bleed turbopump unit for hydrogen propelled nuclear rocket