The purpose of this project is to obtain a conceptional design in which the following topics will be paid attention to: mission profile and possible trajectory; basic geometry; weight and weight distribution; basic avionics; aero(thermo)dynamic loads; lay out of the propulsion system; and costs.
Hypersonic Airbreathing Reusable Advanced Launcher: A Feasibility Study
1993
131 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Astronautics , Manned Spacecraft , Launch vehicles , Aerospace planes , Research projects , Reusable spacecraft , Multistage rocket vehicles , Spacecraft design , Design criteria , Spacecraft structures , Space missions , Spacecraft control , Spacecraft stability , Spacecraft propulsion , Aerodynamics , Hypersonics , Thrust , Systems engineering , Cost analysis , Requirements , Foreign technology , HARALD(Hypersonic Airbreathing Reusable Advanced Launchers)
Hypersonic airbreathing propulsion
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Hypersonic Airbreathing Missile
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