Research Catalog

Title

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

Author

Carson, George T.

Publication

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.

Details

Additional Authors

• Capone, Francis J.
• United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

Description

1 v.

Series Statement

NASA technical memorandum ; 4237

Subject

• Axisymmetric flow
• Convergent-divergent nozzles
• Nozzle design
• Static tests
• Thrust vector control
• Transonic wind tunnels
• Wind tunnel tests

Note

• Distributed to depository libraries in microfiche.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.15:4237

OCLC

marcive32402158

Author

Carson, George T.

Title

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability [microform] / George T. Carson, Jr., and Francis J. Capone.

Imprint

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

NASA technical memorandum ; 4237

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.

Added Author

Capone, Francis J.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.

Gpo Item No.

0830-D (MF)

Sudoc No.

NAS 1.15:4237

Research Call Number

READEX Microfiche NAS 1.15:4237