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Filament wound data base development, revision 1, appendix AData are presented in tabular form for the High Performance Nozzle Increments, Filament Wound Case (FWC) Systems Tunnel Increments, Steel Case Systems Tunnel Increments, FWC Stiffener Rings Increments, Steel Case Stiffener Rings Increments, FWC External Tank (ET) Attach Ring Increments, Steel Case ET Attach Ring Increments, and Data Tape 8. The High Performance Nozzle are also presented in graphical form. The tabular data consist of six-component force and moment coefficients as they vary with angle of attack at a specific Mach number and roll angle. The six coefficients are normal force, pitching moment, side force, yawing moment, axial force, and rolling moment. The graphical data for the High Performance Nozzle Increments consist of a plot of a coefficient increment as a function of angle of attack at a specific Mach number and at a roll angle of 0 deg.
Document ID
19870011582
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sharp, R. Scott
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Braddock, William F.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Subject Category
Space Transportation
Report/Patent Number
NASA-CR-179069
NAS 1.26:179069
LMSC-HREC-TR-D951500-1A
Report Number: NASA-CR-179069
Report Number: NAS 1.26:179069
Report Number: LMSC-HREC-TR-D951500-1A
Accession Number
87N21015
Funding Number(s)
CONTRACT_GRANT: NAS8-35054
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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