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Worldwide Space Launch Vehicles and Their Mainstage Liquid Rocket PropulsionSpace launch vehicle begins with a basic propulsion stage, and serves as a missile or small launch vehicle; many are traceable to the 1945 German A-4. Increasing stage size, and increasingly energetic propulsion allows for heavier payloads and greater. Earth to Orbit lift capability. Liquid rocket propulsion began with use of storable (UDMH/N2O4) and evolved to high performing cryogenics (LOX/RP, and LOX/LH). Growth versions of SLV's rely on strap-on propulsive stages of either solid propellants or liquid propellants.
Document ID
20100015911
Acquisition Source
Stennis Space Center
Document Type
Presentation
Authors
Rahman, Shamim A.
(NASA Stennis Space Center Stennis Space Center, MS, United States)
Date Acquired
August 24, 2013
Publication Date
April 13, 2010
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
SPPT-630-0001
Report Number: SPPT-630-0001
Meeting Information
Meeting: AIAA Greater New Orleans Section Meeting
Location: New Orleans, LA
Country: United States
Start Date: April 13, 2010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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