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This was the first flight of the Saturn I Block II configuration (i.e., lengthened fuel tanks in the S-1 and stabilizing tail fins), as well as the first flight of a live (powered) S-IV upper stage. The S-1, powered by eight H-1 engines, reached a full thrust of over 680,400 kilograms (1.5 million pounds) the first time in flight. The S-IV's 41,000 kilogram (90,000-pound-thrust cluster of six liquid-hydrogen RL-10 engines performed as expected. The Block II SA-5 was also the first flight test of the Saturn I guidance system.
References:
Morse, Mary Louise, and Bays, Jean Kernahan. 1973. The Apollo Spacecraft: A Chronology. Volume II, November 8, 1962-September 30, 1964. NASA SP-4009.
Encyclopedia Astronautica.
Wikipedia.
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