In this report the Faculty of Aerospace Engineering (Faulty LR), TU-Delft, investigates the necessity of space launcher trajectory optimization for the conceptual design of airplane-like space launchers. For this purpose, the Faculty LR acquired in 1994 the highly advanced, German-developed trajectory optimization tool referred to as XGESOP. In this memorandum the capabilities of XGESOP will be demonstrated.
Trajectory Optimization Using XGESOP: Ariane V GTO Trajectory Optimization
1994
52 pages
Report
Keine Angabe
Englisch