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This page is an incomplete list of orbital rocket engine data and specifications. ... Saturn V: 1st RP-1 / LOX ... 5.97: Space Shuttle Solid Rocket Booster [k]
The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program .
The original design of the heavy-lift Ares V, named in homage to the Saturn V, was 360 feet (110 m) in height and featured a core stage based on the Space Shuttle External Tank, with a diameter of 28 feet (8.4 m). It was to be powered by five RS-25 engines and two five-segment Space Shuttle Solid Rocket Boosters (SRBs).
The RS-25 engine consists of pumps, valves, and other components working in concert to produce thrust. Fuel (liquid hydrogen) and oxidizer (liquid oxygen) from the Space Shuttle's external tank entered the orbiter at the umbilical disconnect valves and from there flowed through the orbiter's main propulsion system (MPS) feed lines; whereas in the Space Launch System (SLS), fuel and oxidizer ...
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.
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).
A second space shuttle disaster. Seventeen years after the Challenger disaster, another shuttle and its crew were lost in the skies above America: The shuttle Columbia broke apart upon reentry on ...
The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [69] 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 [ 70 ] Nova was cancelled in 1964 and had reusable ...