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Structural Seal DevelopmentNASA currently has aggressive goals for the development of the next generations of Reusable Launch Vehicles (RLV). Many of the goals center around significantly reducing the time and cost of deployment (including payload) for these spacecraft, as well as substantially increasing the safety of the crew and hardware. A core component in the design of these next generation spacecraft is the propulsion system. Many concepts are currently being evaluated including Rocket Based Combined Cycle (RBCC) and Turbine Based Combined Cycle (TBCC) engine technologies, shown.
Document ID
20030071238
Acquisition Source
Headquarters
Document Type
Other
Authors
DeMange, Jeff
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 7, 2013
Publication Date
October 29, 2002
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
OAI-02-011
Report Number: OAI-02-011
Funding Number(s)
CONTRACT_GRANT: NCC3-879
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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