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The interior of all the Saturn S-Series models received a completely redesigned dashboard, center console, and steering wheel, but the rest of the interiors were mostly unchanged. The SL2, SW2, and SC2 got the storage compartment with a sliding armrest in the center console as standard, whereas the SL1, SW1, and SC1 did not. [9]
The powerplant used in Saturn S-Series automobiles was a straight-4 aluminum piston engine produced by Saturn, a subsidiary of General Motors. The engine was only used in the Saturn S-series line of vehicles (SL, SC, SW) from 1991 through 2002. It was available in chain-driven SOHC or DOHC variants.
The Saturn MP Transmission were a series of 5-speed manual and 4-speed automatic transmissions that were manufactured by Saturn Corporation exclusively for the S-Series.They were designed for transverse engine applications and was deployed in vehicles that output up to 122 ft·lbf of engine torque.
Saturn SC2, a compact sport coupe car; Convoy SC 2, an Allied trade convoy that was attacked during the Second World War; ISO/IEC JTC 1/SC 2, standardization subcommittee for coded character sets; SC2 (leisure complex), in Rhyl; SC02, a FIPS 10-4 region code, see List of FIPS region codes (S–U)
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
The Saturn C-2 was the second rocket in the Saturn C series studied from 1959 to 1962. The design was for a four-stage launch vehicle that could launch 21,500 kg (47,300 lb) to low Earth orbit and send 6,800 kg (14,900 lb) to the Moon via Trans-Lunar Injection .
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.
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.