Research Catalog

Title

Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) [microform] : final report / by Richard H. Sforzini and Jesse E. Murph.

Author

Sforzini, Richard H.

Publication

Auburn, Ala. : Engineering Experiment Station, Auburn University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1980]

Details

Additional Authors

• Murph, Jesse E.
• United States. National Aeronautics and Space Administration.

Description

1 v.

Series Statement

NASA contractor report ; NASA CR-177145

Alternative Title

Solid propellant rocket motor internal ballistics performance variatio analysis (phase five)

Subject

• Applications programs (Computers)
• Booster rocket engines
• Burning rate
• Combustion stability
• Interior ballistics
• Rocket engine design
• Rocket thrust
• Solid propellant combustion
• Solid propellant rocket engines
• Space shuttle boosters
• Thrust distribution

Note

• Distributed to depository libraries in microfiche.

Reproduction (note)

• Microfiche.

Call Number

READEX Microfiche NAS 1.26:177145

OCLC

marcive33339197

Author

Sforzini, Richard H.

Title

Solid-propellant rocket motor internal ballistics performance variatio analysis (phase five) [microform] : final report / by Richard H. Sforzini and Jesse E. Murph.

Imprint

Auburn, Ala. : Engineering Experiment Station, Auburn University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1980]

Series

NASA contractor report ; NASA CR-177145

Reproduction

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 1 microfiche.

Added Author

Murph, Jesse E.

United States. National Aeronautics and Space Administration.

Gpo Item No.

0830-H-14 (MF)

Sudoc No.

NAS 1.26:177145

Research Call Number

READEX Microfiche NAS 1.26:177145