Research Catalog

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability

Title
  1. Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.
Published by
  1. Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
Author
  1. Carson, George T.

Details

Additional authors
  1. Capone, Francis J.
  2. United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Description
  1. 1 v.
Series statement
  1. NASA technical memorandum ; 4237
Subject
  1. Axisymmetric flow
  2. Convergent-divergent nozzles
  3. Nozzle design
  4. Static tests
  5. Thrust vector control
  6. Transonic wind tunnels
  7. Wind tunnel tests
Call number
  1. READEX Microfiche NAS 1.15:4237
Note
  1. Distributed to depository libraries in microfiche.
Reproduction (note)
  1. Microfiche.
Author
  1. Carson, George T.
Title
  1. Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.
Imprint
  1. Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1991.
Series
  1. NASA technical memorandum ; 4237
Reproduction
  1. Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.
Added author
  1. Capone, Francis J.
  2. United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Gpo item no.
  1. 0830-D (MF)
Sudoc no.
  1. NAS 1.15:4237
Research call number
  1. READEX Microfiche NAS 1.15:4237
View in legacy catalog