Launch vehicle dynamic stability characteristics with designed flight control augmentors
36th AIAA Aerospace Sciences Meeting and Exhibit ; 1998 ; Reno , NV , U.S.A.
01.01.1998
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flight Control Augmentors for Aft-Center-of-Gravity Launch Vehicles
Online Contents | 1997
|Launch Vehicle Dynamic Stability Characteristics with Designed Flight Control Augmentors
British Library Conference Proceedings | 1998
|Jet Wing with Multiple Thrust Augmentors
NTIS | 1971
|