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The S-I Saturn stage reached an altitude of 129 kilometers (80 statute miles) and a peak velocity of 5,906 kilometers (3,660 miles) per hour. This was the last of four successful tests for the first stage of the Saturn I vehicle. After 100 seconds of flight, No. 5 of the booster's eight engines was cut off by a preset timer. That engine's propellants were rerouted to the remaining seven, which continued to burn. This experiment confirmed the "engine-out" capability that MSFC engineers had designed into the Saturn I.
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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