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Satan - Alternate name of RM 15A Satan - Alternate name of RM2. Flight record: 1 spaceflight, Flew to orbit on STS Status: Inactive; Active Born: Spaceflights: 1. Total time in space: Launched - Used the AS bus.

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First Launch: Last Launch: Number: 5. Gross mass: kg 1, lb. Launched Number: 7. Gross mass: 1, kg 2, lb.


Number: 2. Gross mass: 1, kg 4, lb. Gross mass: 2, kg 5, lb. Status: Operational Number: 1. Gross mass: 57 kg lb.

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Satelife - American agency. Satelife, USA. Satelind - Indonesian agency. Satelind, Indonesia. Satellite Italiano Ricerca Industriale Orientata - Alternate designation for Sirio communications technology satellite.

Satellite Launch Vehicle - American orbital launch vehicle. Orbital version. Uses half-length shuttle SRB as first stage; proven Castor as second stage; new Castor as third stage; and Orbital Adjustment Module from Lockheed's cancelled Athena launcher as a fourth stage. Payload: 6, kg 13, lb.

Cubesat 2U bus. Gross mass: 2. Satmex - Mexican agency. Used the HSHP bus. Gross mass: 4, kg 9, lb. Used the SSLX bus.

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Gross mass: 5, kg 12, lb. Used the SSL bus. Satrec - The South Korean Satrec Initiative built on earlier Kitsat technology to develop kg and kg satellite buses for national and international customers.

Sattarov, Nail Sharipovich - Tatar-Russian test pilot cosmonaut, Status: Deceased; Active Died: Saturn Saturn - Alternate name for Soyuz Saturn Saturn - Alternate designation for Soyuz Saturn A-1 - American orbital launch vehicle.

Projected first version of Saturn I, to be used if necessary before S-IV liquid hydrogen second stage became available. Titan 1 first stage used as second stage, Centaur third stage. Masses, payload estimated. Status: Study Gross mass:kg 1, lb. Payload: 6, kg 14, lb. Thrust: 6, Saturn A-2 - American orbital launch vehicle.

More powerful version of Saturn I with low energy second stage consisting of cluster of four IRBM motors and tankage, Centaur third stage. Payload: 10, kg 22, lb. Thrust: 7, Saturn B-1 - American orbital launch vehicle.

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Most powerful version of Saturn I considered. Payload: 13, kg 28, lb. Saturn C-1 - American orbital launch vehicle.

Status: Retired Number: 3. Gross mass:kglb. Payload: 9, kg 19, lb. Thrust: 5, Saturn C-1 - Alternate designation for Saturn I. Saturn C-2 - American orbital launch vehicle. The launch vehicle initially considered for realizing the Apollo lunar landing at the earliest possible date. Payload: 21, kg 47, lb. Saturn C-3 - The launch vehicle concept considered for a time as the leading contender for the Earth Orbit Rendezvous approach to an American lunar landing.

Gross mass: 1, kg 2, lb. Payload: 36, kg 80, lb. Thrust: 11, Saturn C-3B - American orbital launch vehicle. Final configuration of the Saturn C-3 at the time of selection of the Semi vl suisse anti aging C-5 configuration for the Apollo program in December Gross mass: 1, kg 3, lb. Payload: 78, kglb. Thrust: 20, Saturn C-3BN - American nuclear orbital launch vehicle.

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Payload: 94, kglb. Saturn C-4 - American orbital launch vehicle. The launch vehicle actually planned for the Lunar Orbit Rendezvous approach to lunar landing. The Saturn C-5 was selected instead to have reserve capacity.

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Gross mass: 2, kg 5, lb. Payload: semi vl suisse anti aging, kglb.

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Thrust: 26, Saturn C-4B - American orbital launch vehicle. Final configuration of the Saturn C-4 at the time of selection of the Saturn C-5 configuration for the Apollo program in December Only Saturn configuration with common bulkhead propellant tanks in first stage, resulting in shorter vehicle than less powerful Saturn C Gross mass: 2, kg 4, lb.

Payload: 95, kglb. Saturn C-5 - American orbital launch vehicle. Final configuration of Saturn C-5 at the time of selection of this configuration for the Apollo program in December The actual Saturn V would be derived from this, but with an increased-diameter third stage 6. Gross mass: 2, kg 6, lb. Payload:kglb.

Very good resistance to fuels Excellent heat resistance Good acid resistance Applications: Due to high chemical resistance and low swelling in fuels especially when containing ethanol and methanol FKM can typically be found in the complete fuel supply chain fuel injectors, quick connectors, high pressure pumps, etc.

Thrust: 33, Saturn C-5N - American nuclear orbital launch vehicle. Saturn C-8 - American orbital launch vehicle. The largest member of the Saturn family ever contemplated. Designed for direct landing of Apollo command module on moon. Configuration used eight F-1 engines in the first stage, eight J-2 engines in the second stage, and one J-2 engine in the third stage.

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Distinguishable from Nova 8L in use of J-2 engines instead of M-1 engines in second stage. Gross mass: 4, kg 10, lb. Thrust: 53, Saturn E-1 - Alternate designation for Super-Jupiter Saturn I - Alternate designation for S-I stage.

Saturn I - American orbital launch vehicle.

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Von Braun launch vehicle known as 'Cluster's Last Stand' - 8 Redstone tanks around a Jupiter tank core, powered by eight Jupiter engines. Originally intended as the launch vehicle for Apollo manned circumlunar flights. However it was developed so early, no payloads were available for it.

Saturn I Blk2 - American orbital launch vehicle. Second Block of Saturn I, with substantially redesigned first stage and large fins to accommodate Dynasoar payload. Number: 9. In the first half of the 's it was planned to make suborbital tests of nuclear propulsion for upper stages using a Saturn IB first stage to boost a Rover-reactor powered second stage on a suborbital trajectory.

The second stage would impact the Atlantic Ocean down range from Cape Canaveral. Status: Development ended Saturn IB - American orbital launch vehicle.

Encyclopedia Astronautica Index: S

Payload: 18, kg 41, lb. Configuration as flown, Saturn IB. Status: Flown Unfuelled mass: 41, kg 91, lb.

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Thrust: 8, Unfuelled mass: 48, kglb. Not found useful in any configuration except with Minuteman first-stage strap-ons to augment thrust.

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