Thermal and chemi-ionization processes in afterburning rocket exhausts.
Mathematical model for thermal and chemi- ionization processes in turbulent nonequilibrium afterburning rocket exhausts plume, studying neutral and charged species distribution
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Mathematical model for thermal and chemi- ionization processes in turbulent nonequilibrium afterburning rocket exhausts plume, studying neutral and charged species distribution
Rocket engine turbopump assembly test capability design, facilities, cryogenic systems, control requirements, computer simulation, activation and checkout
Recirculation zone in fluid mechanics experiments on cylindrical cavity simulating gas-core nuclear rocket as heavy gas reservoir, discussing flow patterns
MIRA 150A variable thrust rocket engine applied to manned lunar exploration flying systems
Fuel consumption precision measurements for low thrust auxiliary rockets using impeller wheel and photometric devices
Preignition phenomena in small Aerozine- 50/nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
Fluidic breadboard version of rocket engine sequence control, describing pneumatic logic package and general limitations
Ionosphere collision frequencies and densities studied by rocket measurements of magnetic field of VLF wave radiated from ground
Electron temperature observation in E region with Langmuir probes on Nike Apache rockets, discussing solar radiation effect
Rocket sampling of noctilucent cloud particles in mesopause
Spectral radiance of model rocket exhaust gases measured by rapid scanning spectrometer at simulated altitude
Early autumn stratospheric circulation of Southern Hemisphere investigated by meteorological rocket observations
Motion equations of spin-stabilized rocket under thrust with jet damping, variable mass and momentum effects and all angular disturbances
Linear segment pitch rate program for near optimum trajectory for rocket boosters
Liquid rocket propellants use in U.S. space program, particularly Apollo project, discussing future trends
Micrometeorite flux rate for Leonid shower measured with Luster sounding rocket collecting surface
Air loads on sounding rocket from distributed aerodynamics and pressure differential
Shock tube simulation of rocket exhaust plumes and effects on vehicles in space environment
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