This article discusses aerodynamic heating, heat protection structures and principles, landing processes, and aircraft-shaped reentry vehicles, satellites, and spacecraft in the reentry process.
The Return of a Satellite and Spacecraft
1977
15 pages
Report
Keine Angabe
Englisch
Heat shields , Heat transfer , Lifting reentry vehicles , Spacecraft Trajectories & Flight Mechanics , Spacecraft , Atmosphere entry , Aerodynamic heating , Reentry vehicles , Unmanned Spacecraft , China , Ablative materials , Thermal radiation , Artificial satellites , Heat sinks , Translations , Aerodynamic configurations
Satellite/spacecraft propulsion
NTRS | 1991
|Mars Sample Return Spacecraft Systems Architecture
British Library Conference Proceedings | 2000
|The Hayabusa Spacecraft Sample Return Mission
NTRS | 2010
|Mars Sample Return Spacecraft Systems Architecture
NTRS | 2000
|