Radiation hazard from backflow of fission fragments from the plume of a gas-core nuclear rocket
Radiation hazard from backflow of fission fragments from plume of gas-core nuclear rocket
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Radiation hazard from backflow of fission fragments from plume of gas-core nuclear rocket
Scaling parameters for simulating highly expanded rocket exhaust plumes and resultant impingement forces on immersed bodies
Research facilities for MA-3 Atlas vernier engine plume property measurement
High altitude scale model experiment to evaluate rocket plume impingement effects on Manned Orbital Workshop pressures, heating rates, forces and moments
Rocket nozzle originated oblique shock waves effect on near-field plume inpingement flows, heat transfer and pressure distribution
Mach disk in underexpanded exhaust plume predicted by dividing flow field into subregions
Particle density of jet plumes exhausting in vacuum calculated for He, Ar and N
Carbon dioxide jet plumes condensation on model nozzle in vacuum chamber, noting particle size and growth rate
ATS-C satellite rocket exhaust plume convective heating measurements of VHF whip antennas, discussing nozzle flow and heating rate
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Optical system measurement of density and rotational temperature in gaseous plume simulating auxiliary propulsion and oxygen hydrogen burner of S-4B
Crew radiation dosage from fission fragments in plume from gas core nuclear rocket
Computer program for resolution band model prediction of heat transfer from rocket exhaust plumes
Space shuttle vehicle rocket plume impingement study for separation analyses
Optimum separation trajectory analysis for two stage space shuttle configuration considering plume impingement effect
Crew radiation dose from plume of high impulse gas-core nuclear rocket during Mars mission
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Mach disk in underexpanded exhaust plume predicted by dividing flow field into subregions