DATO (Descent & Ascent Trajectory Optimisation): From the Launch Pad to Orbit and Back
57th International Astronautical Congress ; 2006 ; Valencia , Spain
01.01.2006
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
ENGINEERING NOTES - Optimal Ascent Trajectory for Efficient Air Launch into Orbit
Online Contents | 2004
|Ascent or Descent from Satellite Orbit by Low Thrust
AIAA | 1966
|Ascent or descent from satellite orbit by low thrust
Engineering Index Backfile | 1966
|