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165 + 335 seconds (2 burns) Propellant. LH 2 / LOX. [ edit on Wikidata] The Saturn V [a] is a retired American super heavy-lift launch vehicle developed by NASA under the Apollo program for human exploration of the Moon. The rocket was human-rated, had three stages, and was powered by liquid fuel.
The General Dynamics Nexus was proposed in the 1960s as a fully reusable successor to the Saturn V rocket, having the capacity of transporting up to 450–910 t (990,000–2,000,000 lb) to orbit. The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket.
A Saturn V rocket, one of the most powerful operational launch vehicles to date. This article compares different orbital launcher families (launchers which are significantly different from other members of the same 'family' have separate entries).
This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets.
Burn time. 150 s. Propellant. RP-1 / LOX. The S-IC (pronounced S-one-C [2] [3]) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, most of its mass of more than 2,000 t (4,400,000 lb) at launch was propellant, in this case RP-1 rocket fuel and liquid ...
Launch Vehicle Digital Computer. The Launch Vehicle Digital Computer ( LVDC) was a computer that provided the autopilot for the Saturn V rocket from launch, through Earth orbit insertion, and the trans-lunar injection burn that would send the Apollo spacecraft to the Moon. Designed and manufactured by IBM 's Electronics Systems Center in Owego ...
J002E3 is in the circle. Computer simulation of J002E3's motion, alternating between six Earth orbits and a heliocentric orbit (click on image to view animation) S-IVB stage of Apollo 17. The one used for Apollo 12 is of identical type. J002E3 is an object in space which is thought to be the S-IVB third stage of the Apollo 12 Saturn V rocket.
Three variants of the Saturn family which were developed: Saturn I, Saturn IB, and Saturn V. The Saturn family of American rockets was developed by a team of former German rocket engineers and scientists led by Wernher von Braun to launch heavy payloads to Earth orbit and beyond. The Saturn family used liquid hydrogen as fuel in the upper stages.