Research Catalog

Title

High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment [microform] : final report / prepared by J.A. Freeman ... [et al.].

Publication

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]

Details

Additional Authors

• Freeman, Jon A.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA contractor report ; NASA CR-179307

Subject

• Erosion
• Flow distribution
• Gas dynamics
• Naver-Stokes equation
• Nozzle geometry
• Rocket nozzles
• Space shuttle boosters

Note

• Distributed to depository libraries in microfiche.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.26:179307

OCLC

marcive33099178

Title

High performance solid rocket motor (SRM) submerged nozzle-combustion cavity flowfield assessment [microform] : final report / prepared by J.A. Freeman ... [et al.].

Imprint

[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]

Series

NASA contractor report ; NASA CR-179307

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1988] 1 microfiche.

Added Author

Freeman, Jon A.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-H-14 (MF)

Sudoc No.

NAS 1.26:179307

Research Call Number

READEX Microfiche NAS 1.26:179307