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Maximum thrust: 34,500 kN (7,750,000 lbf) sea ... It was a Saturn V derived launch vehicle with over twice the payload capability and would have relied completely on ...
To date, the Saturn V is the only launch vehicle from the Apollo Space Program to transport human beings beyond low Earth orbit. A total of 24 humans were flown to the Moon in the four years spanning December 1968 through December 1972.
The S-IC (pronounced S-one-C [3] [4]) 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, more than 90% of the mass at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer.
Diagram of Saturn V Launch Vehicle. The Saturn V consisted of three stages and an Instrument Unit (IU). The first stage, S-IC, delivered 7,610,000 pounds-force (33.9 MN) thrust and delivered the other stages to 200,000 feet (61 km). [12] Afterwards, it was jettisoned to fall into the Atlantic Ocean and the second stage continued acceleration. [12]
While outwardly very similar to the F-1, the F-1A produced about 20% greater thrust, 1,800,000 lbf (8 MN) in tests, and would have been used on future Saturn V vehicles in the post-Apollo era. However, the Saturn V production line was closed prior to the end of Project Apollo and no F-1A engines ever flew. [10]
The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [71] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [ 72 ] Nova was cancelled in 1964 and had reusable ...
The S-II (pronounced "S-two") was the second stage of the Saturn V rocket. It was built by North American Aviation. Using liquid hydrogen (LH2) and liquid oxygen (LOX) it had five J-2 engines in a quincunx pattern. The second stage accelerated the Saturn V through the upper atmosphere with 1,000,000 pounds-force (4.4 MN) of thrust.
A 1968 proposal for a Saturn V ELV (MLV-SAT-V-25(S)U) According to the 1968 NASA document "Integrated Manned Interplanetary Spacecraft Concept Definition", there was a planned schedule for exploration under the ELV program. [2] After the first crewed Apollo lunar landing, NASA was hoping to progress through the following list: