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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.
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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.
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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. 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. 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 achat flash ball suisse anti aging 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.
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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. Most powerful version of Saturn I considered.
Wardnak a Fekete Tőr Testvériségről szóló regénysorozata: az egyik vámpír harcos átlépi az életet a haláltól elválasztó határvonalat, ezzel a sötét fantáziák és még sötétebb vágyak erotikus világába kerül. Várandós felének tragikus halála óta Tohrment csak árnyéka önmagának. Testileg megtörve, lelkileg szinte megsemmisülve kerül vissza a testvériség házába, egy bukott angyal, Lassiter segítségével.
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.
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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. Payload: 78, kglb.
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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.
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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, kg 6, lb.
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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. 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. Von Braun launch vehicle known as 'Cluster's Last Stand' - 8 Redstone tanks around a Jupiter tank core, powered by eight Jupiter engines.
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However it was developed so early, no payloads were available for it. Saturn I Blk2 - American orbital launch vehicle.
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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 achat flash ball suisse anti aging 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. Payload: 18, kg 41, lb. Configuration as flown, Saturn IB. Status: Flown Unfuelled mass: 41, kg 91, lb. Thrust: 8, Unfuelled mass: 48, kglb. Not found useful in any configuration except with Minuteman first-stage strap-ons to augment thrust. Unfuelled mass: 45, kglb.
Saturn IB-B - American orbital launch vehicle.
