Low thrust trajectory analyses were used to examine the feasibility of using solar electronic propulsion for Earth escape from a negative C3 launch for deep space missions in order to significantly increase the net delivered mass capability of inexpensive launch vehicles.
Negative C3 Launch Options for Solar System Exploration
Joint Propulsion Conference
13.07.1998
Aufsatz (Konferenz)
Keine Angabe
Englisch
Negative C3 launch for solar system exploration
AIAA | 1998
|Launch Vehicle Options for Exploration
British Library Conference Proceedings | 2004
|Launch Vehicle Options for Exploration
British Library Conference Proceedings | 2004
|