IAF92-0622 - IAF92-0685International Astronautical Federation, 1992 - Astronautics |
Common terms and phrases
43rd CONGRESS AIAA ARIANE ASTRONAUTICAL FEDERATION August ATREX binder boosters capability chamber pressure coefficient combustion chamber component configuration cooling copy or republish cost cryogenic cycle DC For permission density diameter droplet efficiency FEDERATION August 28-September Figure flame flight fuel heat exchanger heat transfer HTPB hybrid rocket hydrogen ignition increase injection injectors inlet interface International Astronautical Federation Laboratory launch vehicle liquid Mach mass mission mixture ratio module NASA nozzle O/F ratio operation orbit oxidizer parameters payload performance phase plug engine plume diagnostics propulsion system Propulsion Technology pump reliability rhenium rocket engine Scramjet shown solid propellant solid rocket motor SPACE CONGRESS 1992 Space Shuttle Space Station spacecraft specific impulse SSME SSTO stage staged combustion cycle tank temperature thermal thermal insulation thrust chamber thruster turbine turbopump turbulent vapor velocity weight WORLD SPACE CONGRESS