DATO (Descent & Ascent Trajectory Optimisation): From the Launch Pad to Orbit and Back
57th International Astronautical Congress ; 2006 ; Valencia , Spain
2006-01-01
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 TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION
British Library Conference Proceedings | 2012
|