TY  - RPRT
TI  - Space Shuttle main engine powerhead structural modeling, stress and fatigue life analysis. Volume 3: Stress summay of blades and nozzles at FPL and 115 percent RPL loads. SSME HPFTP and HPOTP blades and nozzles
AU  - Hammett, J. C.
AU  - Hayes, C. H.
AU  - Price, J. M.
AU  - Robinson, J. K.
AU  - Teal, G. A.
AU  - Thomson, J. M.
AU  - Tilley, D. M.
AU  - Welch, C. T.
PY  - 1983
UR  - https://ntrs.nasa.gov/citations/19840012569
ID  - 19840012569
ER  -