Thruster exhaust effects upon spacecraft
Thruster exhaust effects on spacecraft structures
SEARCH · Search NASA
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Thruster exhaust effects on spacecraft structures
Design and characteristics of exhaust system for supersonic aircraft
Analytic functions and fluid mechanics for noise propagation in supersonic jet exhaust flow
Wind tunnel tests to determine effects of retrorocket exhaust on drag of 120 deg cone at subsonic speeds
Reductions in smoke level and carbon monoxide emissions resulting from air-assist fuel nozzles in jet aircraft exhaust pollutant tests
Use of air-assist fuel nozzle to reduce exhaust emissions from gas turbine combustor at simulated idle conditions - J-57 engine
Comparison of predicted and experimental wall temperature for cylindrical ejector exhaust nozzle operated with turbojet gas generator
Rocket exhaust cloud mass-energy balance measurements for Saturn S1-C static firing
Flow characteristics in exhaust of pulsed megawatt gas fed arc examined with piezoelectric pressure tranducer
Exhaust jet mixing flow nozzles with peak axial velocity degradation for noise suppression
Effects of exhaust deposits from 22.5 newton thrust, bipropellant, attitude control engine on transmittance in 0.2 to 0.6 and 0.32 to 2.2 micron ranges
Low speed wind tunnel tests of takeoff, landing, and cruise aerodynamic characteristics of space shuttle booster with exhaust effect simulation
Spacecraft propellant condensation on low temperature surfaces near cesium ion thruster exhaust, considering neutral atoms impingement and charge exchange
Internal combustion engine exhaust system sound radiation, discussing pressure wave effects, energy flux and boundary conditions
Pulsed megawatt MPD arc thruster exhaust pressure measurements, discussing time dependence, peak dynamic and static pressures, etc
Lanthanum cobalt oxide as potential auto exhaust catalyst from studies of activity in gas phase
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