Abstract The possibility of using an inflatable braking device for controlled descent in the Martian atmosphere of large-capacity cargoes is analyzed. The most complicated version of the trajectory control problem is considered, namely, the injection of a spacecraft at hyperbolic velocity into a parking orbit after braking in the atmosphere.
Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere
Cosmic Research ; 41 , 3
2003
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.60 Raumfahrttechnik / 39.00 Astronomie: Allgemeines / 50.93 Weltraumforschung | |
Lokalklassifikation TIB: | 770/3520/8000 |
Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere
Springer Verlag | 2003
|Foam-Reinforced Inflatable Spacecraft
Online Contents | 1997