Saturn C-8
Encyclopedia
The Saturn C-8 was the largest member of the Saturn series of rockets to be designed. It was a potential alternative to the Nova rocket, should NASA
have chosen a direct-landing method of lunar exploration
for the Apollo program. The first stage was an increased diameter version of the S-IC
. The second stage was an increased diameter S-II
stage. Both of these stages had eight engines, as opposed to the standard five. The third stage was a stretched S-IVB
stage, which retained its original diameter and engine.
Ultimately, the Lunar Orbit Rendezvous
("LOR") concept rendered the C-8 obsolete, and the smaller Saturn C-5 was developed instead under the designation "Saturn V
", as the LOR spacecraft was within its payload capacity.
The C-8 was never taken further than the design process as it was too large and costly.
NASA
The National Aeronautics and Space Administration is the agency of the United States government that is responsible for the nation's civilian space program and for aeronautics and aerospace research...
have chosen a direct-landing method of lunar exploration
Exploration of the Moon
The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation. The invention of the optical telescope brought about the...
for the Apollo program. The first stage was an increased diameter version of the S-IC
S-IC
The S-IC was the first stage of the Saturn V rocket. The S-IC first stage was built by The Boeing Company. Like the first stages of most rockets, most of its mass of over two thousand metric tonnes at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen oxidizer...
. The second stage was an increased diameter S-II
S-II
The S-II was the second stage of the Saturn V rocket. It was built by North American Aviation. Using liquid hydrogen and liquid oxygen it had five J-2 engines in a cross pattern...
stage. Both of these stages had eight engines, as opposed to the standard five. The third stage was a stretched S-IVB
S-IVB
The S-IVB was built by the Douglas Aircraft Company and served as the third stage on the Saturn V and second stage on the Saturn IB. It had one J-2 engine...
stage, which retained its original diameter and engine.
Ultimately, the Lunar Orbit Rendezvous
Lunar orbit rendezvous
Lunar orbit rendezvous is a key concept for human landing on the Moon and returning to Earth.In a LOR mission a main spacecraft and a smaller lunar module travel together into lunar orbit. The lunar module then independently descends to the lunar surface. After completion of the mission there, a...
("LOR") concept rendered the C-8 obsolete, and the smaller Saturn C-5 was developed instead under the designation "Saturn V
Saturn V
The Saturn V was an American human-rated expendable rocket used by NASA's Apollo and Skylab programs from 1967 until 1973. A multistage liquid-fueled launch vehicle, NASA launched 13 Saturn Vs from the Kennedy Space Center, Florida with no loss of crew or payload...
", as the LOR spacecraft was within its payload capacity.
The C-8 was never taken further than the design process as it was too large and costly.