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Status of Nozzle Aerodynamic Technology at MSFCThis viewgraph presentation provides information on the status of nozzle aerodynamic technology at MSFC (Marshall Space Flight Center). The objectives of this presentation were to provide insight into MSFC in-house nozzle aerodynamic technology, design, analysis, and testing. Under CDDF (Center Director's Discretionary Fund), 'Altitude Compensating Nozzle Technology', are the following tasks: Development of in-house ACN (Altitude Compensating Nozzle) aerodynamic design capability; Building in-house experience for all aspects of ACN via End-to-End Nozzle Test Program; Obtaining Experimental Data for Annular Aerospike: Thrust eta, TVC (thrust vector control) capability and surface pressures. To support selection/optimization of future Launch Vehicle propulsion we needed a parametric design and performance tool for ACN. We chose to start with the ACN Aerospike Nozzles.
Document ID
20030000739
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ruf, Joseph H.
(NASA Marshall Space Flight Center Huntsville, AL United States)
McDaniels, David M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Smith, Bud
(Plumetech Huntsville, AL United States)
Owens, Zachary
(Virginia Univ. Hampton, VA United States)
Date Acquired
August 21, 2013
Publication Date
July 1, 2002
Publication Information
Publication: Twelfth Thermal and Fluids Analysis Workshop
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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