Modelling of jet impingement forces during hot stage-separation of a launch vehicle
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit ; 1998 ; Cleveland , OH , U.S.A.
1998-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Reusable Launch Vehicle having Non-Explosive Stage Separation Device
Europäisches Patentamt | 2024
|