A general trajectory scenario has been designed which can transfer a spacecraft from a pre-specified, highly eccentric, near equatorial orbit to a desired escape direction.
Venus and Beyond Using the Ariane ASAP Launch Capability
1999-08-16
Miscellaneous
No indication
English
Venus and Beyond Using the Ariane ASAP Launch Capability
NTRS | 1999
|Venus and Beyond Using the Ariane ASAP Launch Capability (AAS 99-357)
British Library Conference Proceedings | 2000
|Venus and Beyond Using the Arine ASAP Launch Capability
NTRS | 1999
|Mission Design for Mars Missions Using the Ariane ASAP Launch Capability
British Library Conference Proceedings | 1999
|