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

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Gross mass: 1, kg 4, lb. Gross mass: 2, kg 5, lb. Status: Operational Number: 1. Gross mass: 57 kg lb. Satelife - American agency. Satelife, USA. Satelind - Indonesian agency.

Encyclopedia Astronautica Index: S

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

Satellite Launch Vehicle - American orbital launch vehicle.

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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.

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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. 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.

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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.

Svájci szövetségi tanácsadó anti aging 10, kg 22, lb. Thrust: 7, Saturn B-1 - American orbital launch vehicle. Most powerful version of Saturn I considered. Payload: 13, kg 28, lb.

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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. Fotóradar mobil suisse anti aging 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: fotóradar mobil suisse anti aging, 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. 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. Gross mass: 2, kg 5, lb. 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. Final configuration of Saturn C-5 at the time of selection of this configuration for the Apollo program in December