Multiple impulsive spacecraft trajectory optimization technique application to comet rendezvous problem, using computer program
Application of an impulsive trajectory optimization method to the comet rendezvous problem
AEROSPACE SCIENCES MEETING ; 1971 ; NEW YORK, NY
1971-01-01
Conference paper
No indication
English
Trajectory requirements for comet rendezvous
AIAA | 1970
|Trajectory requirements for comet rendezvous
NTRS | 1970
|Trajectory Requirements for Comet Rendezvous
AIAA | 1971
|