Inviscid analysis of the plume created by multiple rocket engines. Part II - Description of the computer programs
Computer program for calculation of single jet and five jet interaction regimes associated with multiple rocket engines
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Computer program for calculation of single jet and five jet interaction regimes associated with multiple rocket engines
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Mass loading effects on localized vibratory environments of rocket vehicles
Effect of fuel opacity on temperature distribution in gaseous nuclear rocket engine
Secondary water flow rates in vertical diffuser of decreasing length using rocket exhaust jet as motive fluid - model sound compressor
Thin film, heat flux probe for measuring gas velocities in unstable rocket combustor
Measurements of gamma and neutron dose distributions in core of thermal tungsten nuclear rocket experiment
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Celestial observation, sounding rocket data, and emission spectrum used to identify Sco X-1 of Scorpio constellation
Subliming solid propellant attitude control rocket
Meteoroid hazards to solid propellant rocket motors
Development of 260-inch diameter solid propellant rocket motor