The Saturn V F-1 engine revisitedThis paper describes how the Saturn V F-1 engine could be resurrected for potential use in a new heavy lift launch vehicle (HLLV). Performance, history, and reliability of the F-1 will be discussed and a 1990s F-1 engine configuration presented. The status of residual hardware, production capability, test-stand availability, and a general program plan to accomplish this restart will be presented. Similarities between restarting the F-1 program and restarting the Atlas and Delta engine programs will be discussed.
Document ID
19920056018
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shelton, B. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Murphy, T. (Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)