Trajectory control logic of space exploration rocket required to arrive given site with zero speed at given time
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 31 , 3 ; 265-269
2005-01-01
5 pages
Article (Journal)
Unknown
DDC: | 629.4 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Minimum Weight Engine Configuration Given Required Power
AIAA | 2019
|Design Opportunities Given Zero Failure Eelectronics
SAE Technical Papers | 2002
|Design opportunities given zero failure electronics
Automotive engineering | 2002
|MINIMUM WEIGHT ENGINE CONFIGURATION GIVEN REQUIRED POWER
TIBKAT | 2019
|