Space shuttle main engine powerhead structural modeling, stress and fatigue life analysis
By: prepared for National Aeronautics and Space Administration, Marshall Space Flight Center by J.C. Hammett ... [et al.].
Contributors: Hammett, J. C.
Series: NASA-CR-170999-171002; NASA contractor report -- NASA CR-170999-171002.
Publisher: Lockheed Missiles & Space Company, Huntsville Research & Engineering Center; Marshall Space Flight Center
Published: 1983
Place of publication: Huntsville, Ala
Language: eng
Format: Microform
Subjects: Gas dynamics.; Turbines -- Blades.; Thermal stresses.; Thermodynamics.
Notes: Distributed to depository libraries in microfiche; shipping list no. not available.

"December 1983."

Contract no. NAS 8-34978.

Includes bibliographical references.

Microfiche. [Washington, D.C. : National Aeronautics and   Space Administration, 1983] 10 microfiches : negative.
Table of contents: title: v. 1. Gasdynamic environment of the SSME HPFTP and HPOTP turbines; title: v. 2. Dynamics of blades and nozzles SSME HPFTP and HPOPT; title: v. 3. Stress summary of blades and nozzles at FPL and 115 percent RPL loads, SSME HPFTP and HPOTP blades and nozzles; title: v. 4. Summary of investigation of unscheduled events and special tasks.