Integration of Vehicle, Propulsion System and Separation Unit Designs for a Launcher Using in-flight Oxygen Collection
AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference
2005-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Propulsion vehicle integration for reusable launcher using in-flight oxygen collection
Online Contents | 2008
|Propulsion vehicle integration for reusable launcher using in-flight oxygen collection
Online Contents | 2008
|