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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.
User:Evan/Budapest - Wikitravel
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 dubied covet suisse anti aging 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.
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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.
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.
Of course, this does not mean that we have to agree on everything, and we have expressed our concerns about some of the recent political developments in Hungary, but we have also acknowledged when the government took important steps to remedy these shortcomings.
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. 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 Saturn C-5 configuration for the Apollo program in December