Determination of launch vehicle trajectory dispersions.
MOCH, T. K. /DOUGLAS AIRCRAFT CO., INC., MISSILE AND SPACE SYSTEMS DIV., FLIGHT MECHANICS DEPT., SAN
JOURNAL OF SPACECRAFT AND ROCKETS ; 3 , 11 ; 1682-1685
1966
Article (Journal)
Electronic Resource
English
Hybrid Launch Vehicle Trajectory Assumptions Analysis
AIAA | 2012
|HYBRID LAUNCH VEHICLE TRAJECTORY ASSUMPTIONS ANALYSIS
British Library Conference Proceedings | 2012
|Trajectory optimization for an asymmetric launch vehicle
NTRS | 1990
|AS-202 launch vehicle operational flight trajectory
NTRS | 1966
|