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The largest production model of the Saturn family of rockets, the Saturn V was designed under the direction of Wernher von Braun at the Marshall Space Flight Center in Huntsville, Alabama; the lead contractors for construction of the rocket were Boeing, North American Aviation, Douglas Aircraft Company, and IBM. Fifteen flight-capable vehicles ...
The final launch of Saturn V in 1973 placed Skylab, a 77-tonne (170,000 lb) payload, into LEO. The Energia launcher was designed by the Soviet Union to launch up to 105 t (231,000 lb) to low Earth orbit. [ 8 ]
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:
Maximum payload mass (kg) Reusable / Expendable Orbital launches including failures [a] Suborbital test flights Launch site(s) Dates of flight LEO GTO Other First Latest Starship Block 1 [140] United States: SpaceX: 121 m 40,000 – 50,000 [141] N/A N/A Reusable: 0 6 Starbase: 2023 2024 Angara A5 / Orion Russia: Khrunichev: 54.9 m N/A 6,500 ...
The payload fraction is the quotient of the payload mass and the total vehicle mass at the start of its journey. ... Apollo 17 Saturn V [3] 2,961,860 kg 48,609 kg to ...
With use of the Saturn V vehicle during Apollo, NASA began considering plans for a hypothesized evolutionary Saturn V family concept that spans the earth orbital payload spectrum from 50,000 to over 500,000 lbs.
The Saturn C-5 (later given the name Saturn V), the most powerful of the Silverstein Committee's configurations, was selected as the most suitable design. At the time the mission mode had not been selected, so they chose the most powerful booster design in order to ensure that there would be ample power. [ 24 ]
The S-IVB (pronounced "S-four-B") was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles. Built by the Douglas Aircraft Company, it had one J-2 rocket engine. For lunar missions it was fired twice: first for Earth orbit insertion after second stage cutoff, and then for translunar injection (TLI).