Saturn I/IB/V Launch Vehicle Flight History by Variant/Year (1961-1975) Page 1 of 1 L(F) = Number of Launches(Number of Failures) Saturn I Saturn I Saturn IB Saturn V Orbital All Block I* Block II Totals Totals Year L(F) L(F) L(F) L(F) L(F) L(F) ----------------------------------------------------------------- 1960 - - - - - - 1961 1(0)* - - - - 1(0) 1962 2(0)* - - - - 2(0) 1963 1(0)* - - - - 1(0) 1964 - 3(0) - - 3(0) 3(0) 1965 - 3(0)+ - - 3(0) 3(0) 1966 - - 3(0)# - 1(0) 3(0) 1967 - - - 1(0) 1(0) 1(0) 1968 - - 2(0) 2(1)% 4(1) 4(1) 1969 - - - 4(0) 4(0) 4(0) 1970 - - - 1(0)++ 1(0) 1(0) 1971 - - - 2(0) 2(0) 2(0) 1972 - - - 2(0) 2(0) 2(0) 1973 - - 3(0) 1(0)$ 4(0) 4(0) 1974 - - - - - - 1975 - - 1(0) - 1(0) 1(0) 1976 - - - - - - 1977 - - - - - - 1978 - - - - - - 1979 - - - - - - -------------------------------------------------------------------- Saturn I Saturn I Saturn IB Saturn V Orbital All Block I* Block II Totals Totals Year L(F) L(F) L(F) L(F) L(F) ------------------------------------------------------------------- Suborb 4(0) - 2(0) - - 6(0) Orbit - 6(0) 7(0) 13(1) - 26(1) Total 4(0) 6(0) 9(0) 13(1) - 32(1) ------------------------------------------------------------------ Footnotes: * Suborbital Flights of Saturn I Block I tested S-I stage only, carried dummy S-IV and S-V upper stages + SA-8 flew successful orbital mission despite having one of eight S-I stage engines shut down near end of first stage burn. # Two 1966 suborbital Saturn IB test flights (AS-201, AS-202) carried live S-IVB stages and Apollo CSMs. % SA-502 (Apollo 6) flight suffered pogo oscillations that damaged the SLA, caused two S-II J-2 engines to shut down early, and caused the S-IVB J-2 engine restart to fail, leaving Apollo 6 in a 175 by 356 km low earth orbit, far short of the planned 185 by 528,000 km elliptical orbit. A backup-plan SM engine burn allowed Apollo 6 to achieve some mission objectives despite the launch vehicle failure. ++ SA-508 (Apollo 13) suffered a shutdown of the S-II stage center J-2 engine during ascent due to a pogo oscillation, but still achieved orbit. The problem did not hamper the mission, but the failure was nearly catastrophic. $ SA-513, the final Saturn V, used only two stages to boost Skylab directly into low earth orbit. Saturn Launch Vehicle Flight Evaluation Reports, Marshall Space Flight Center, 1962-1975. Jonathan's Space Report Launch Vehicle Database "http://www.planet4589.org/space/lvdb/index.html" Encylopedia Astronautica "http://www.astronautix.com/" Gunter's Space Page "http://www.skyrocket.de/space" TRW Space Logs, 1957-1996. Last Update 12/8/2003 by Ed Kyle