Particle-in-cell simulations of Hall thruster acceleration and near plume regions
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Computer program determines the radiant flux to the base region of a real gas system with an axisymmetric geometry and any axisymmetric property distribution.
Methods for predicting radiative base heating by hot water vapor in rocket exhaust gases
Rocket exhaust research in areas of direct impingement heating, backwash base heating, radio signal attenuation, and interference with line of sight to ground stations
Measurement of absorptivity and fine structure parameters of water vapor for use in evaluating radiative base heating of Saturn 5 launch vehicles
Computer program manual to analyze loads and heating on bodies subject to rocket exhaust impingement
Apollo telescopic experiment contamination by space vehicle exhaust products
Impingement loadings on Saturn 5 workshop cluster arrangement due to command service module reaction control motor
Experimental study of measuring gas number density in near flow field of low density rocket exhaust at high altitude
Calculation of crew radiation dosage from uranium gas nuclear rocket engine exhaust backflow of fission products