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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: 3900 fr suisse anti aging Spaceflights: 1.

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Total time in space: Launched - Used the AS bus. First Launch: Last Launch: Number: 5.

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Gross mass: kg 1, lb. Launched Number: 7. Gross mass: 1, kg 2, lb.

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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.

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Satelind, Indonesia. Satellite Italiano Ricerca Industriale Orientata - Alternate designation for Sirio communications technology satellite.

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Satellite Launch Vehicle - American orbital launch vehicle. Orbital version.

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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.

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Gross mass: 2. Satmex - Mexican agency.

Used the HSHP bus. Gross mass: 4, kg 9, lb. Used the SSLX bus. 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.

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Sattarov, Nail Sharipovich - Tatar-Russian test pilot cosmonaut, Status: Deceased; Active Died: Saturn Saturn - Alternate name for Soyuz Saturn Saturn - Alternate 3900 fr suisse anti aging 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.

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Masses, payload estimated. Status: Study Gross mass:kg 1, lb. Payload: 6, kg 14, lb.

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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.

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Thrust: 7, Saturn B-1 - American orbital launch vehicle. 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.

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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 Saturn C-5 configuration for the Apollo program in December Gross mass: 1, kg 3, lb.

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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.

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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. Gross mass: 2, kg 5, gault millau 2020 suisse anti aging. Payload: 99, kglb.

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.

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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, 3900 fr suisse anti aging 6, lb. Payload:kglb. 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.