This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
S-100 - Spacecraft - Manned -
Space Suits - USA
S-1029 - Spacecraft - Manned -
Space Suits - USA
S-155 - Rocket Engine - Russia - propellants - 4,000 kgf
S-15 - Spacecraft - Solar -
- USA
S-1 - Spacecraft - Earth -
Magnetosphere - USA
S-2 Pressure Suit - Spacecraft - Manned -
Space Suits - USA
S-2 - Spacecraft - Earth -
Magnetosphere - USA
S-3-20M5A - Rocket Engine - Russia - Nitric acid/Kerosene propellants - kgf
S-30 - Spacecraft - Earth -
Ionosphere - USA
S-3D - Rocket Engine - - Lox/Kerosene propellants - kgf - See S-3D
S-3 - Rocket Engine - USA - Lox/Kerosene propellants - 77,367 kgf
S-40TM - Rocket Engine - Brazil - Solid propellants - 212,500 kgf
S-43 - Rocket Engine - Brazil - Solid propellants - 309,000 kgf
S-43TM - Rocket Engine - Brazil - Solid propellants - 327,000 kgf
S-44 - Rocket Engine - Brazil - Solid propellants - 33,900 kgf
S-46 - Spacecraft - Earth -
Magnetosphere - USA
S-4 - Spacecraft - Manned -
Space Suits - USA
S-55 - Spacecraft - Earth -
Micrometeoroid - USA
S-56 - Spacecraft - Earth -
Atmosphere - USA
S-939 - Spacecraft - Manned -
Space Suits - USA
S-IVB Advanced Station - Spacecraft - -
-
S09.29 - Rocket Engine - Russia - Nitric acid/Amine propellants - 9,000 kgf
S1.35800 - Rocket Engine - Russia - Lox/Kerosene propellants - 3,100 kgf
S1.5400A - Rocket Engine - Russia - Lox/Kerosene propellants - 6,860 kgf - See S1.5400A
S1.5400 - Rocket Engine - Russia - Lox/Kerosene propellants - 6,670 kgf - See S1.5400
S1010 - Spacecraft - Manned -
Space Suits - USA
S1024B - Spacecraft - Manned-
Space Suits - USA - See A/P22S-6A
S1024 - Spacecraft - Manned-
Space Suits - USA - See A/P22S-6
S1030A - Spacecraft - Manned-
Space Suits - USA - See EES
S1030 - Spacecraft - Manned -
Space Suits - USA
S1031 - Spacecraft - Manned -
Space Suits - USA
S1032 - Spacecraft - Manned-
Space Suits - USA - See Shuttle LES
S1034 - Spacecraft - Manned -
Space Suits - USA
S1035 - Spacecraft - Manned-
Space Suits - USA - See ACES
S1035X - Spacecraft - Manned-
Space Suits - USSR - See D-1
S1 - Rocket Stage - Ukraine - Lox/UDMH - 8,595 kg - See Kosmos A-2
S2.1100 - Rocket Engine - Russia - propellants - kgf
S2.1150 - Rocket Engine - Russia - Nitric acid/Amine propellants - 68,440 kgf - See S2.1150
S2.1200 - Rocket Engine - Russia - propellants - kgf - See S2.1200
S2.145 - Rocket Engine - Russia - propellants - 9,000 kgf
S2.253 derivative - Rocket Engine - Russia - Lox/Kerosene propellants - 10,945 kgf
S2.253A - Rocket Engine - Russia - Nitric acid/Kerosene propellants - 9,500 kgf - See S2.253A
S2.253 - Rocket Engine - Russia - Nitric acid/Kerosene propellants - 9,514 kgf - See S2.253
S2.713 - Rocket Engine - Russia - Nitric acid/Amine propellants - 25,717 kgf
S2.720 - Rocket Engine - Russia - Nitric acid/Amine propellants - 3,498 kgf - See S2.720
S2.721V - Rocket Engine - Russia - Nitric acid/Amine propellants - 1,200 kgf - See S2.721V
S3.42A - Rocket Engine - Russia - propellants - 17,000 kgf
S3 - Rocket Stage - Ukraine - Nitric acid/UDMH - 20,135 kg - See Kosmos-2
S5.19 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 200 kgf - See KDU-414
S5.1 - Rocket Engine - Russia - Nitric acid/Amine propellants - 17,000 kgf
S5.23, D-25 - Rocket Engine - Ukraine - N2O4/UDMH propellants - 8,026 kgf - See RD-861
S5.23 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 16,060 kgf - See 11D49
S5.35 + S5.60 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 417 kgf - See KTDU-35
S5.3 - Rocket Engine - Russia - Nitric acid/Amine propellants - 40,000 kgf
S5.3M - Rocket Engine - Russia - Nitric acid/Amine propellants - 40,452 kgf - See S5.3M
S5.44 - Rocket Engine - Russia - Nitric acid/Amine propellants - 18,000 kgf - See S5.44
S5.45 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 200,000 kgf
S5.4 - Rocket Engine - Russia - Nitric acid/Amine propellants - 1,614 kgf - See S5.4
S5.5, S5.5A - Rocket Engine - Russia - Nitric acid/Amine propellants - 4,643 kgf - See KTDU-5A
S5.51 - Rocket Engine - Russia - N2O4/UDMH propellants - 3,388 kgf - See S5.51
S5.53 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 417 kgf - See KTDU-53
S5.61 - Rocket Engine - Russia - N2O4/UDMH propellants - 1,918 kgf - See KRD-61
S5.66 - Rocket Engine - Russia - Nitric acid/UDMH propellants - 417 kgf - See KTDU-66
S5.79 - Rocket Engine - Russia - N2O4/UDMH propellants - 315 kgf - See KRD-79
S5.80.1100-0 - Rocket Engine - Russia - Lox/Kerosene propellants - 300 kgf
S5.80 - Rocket Engine - Russia - N2O4/UDMH propellants - 632 kgf - See KTDU-80
S5.92 - Rocket Engine - Russia - N2O4/UDMH propellants - 2,000 kgf - See S5.92
S5.98M - Rocket Engine - Russia - N2O4/UDMH propellants - 2,000 kgf - See S5.98M
S73-7 Cal Balloon - Spacecraft - Calibration -
- USA
S80/T - Spacecraft - Technology -
Communications - France
S901/970 - Spacecraft - Manned -
Space Suits - USA
SA-1 - Launch Vehicle -
SA-200HP - Spacecraft - Planetary-
Asteroid - USA - See Deep Space 1
SAC-A - Spacecraft - Technology -
- Argentina
SAC-B - Spacecraft - Solar -
- Argentina
Sacco - Dr Albert Sacco Jr - American Astronaut - Payload Specialist
SACI - Spacecraft - Technology -
- Brazil
SAC - Space Project - Astronomy -
Saenger II - Launch Vehicle - Germany
Saenger I - Launch Vehicle -
Saenger - Launch Vehicle - Germany
Safir - Spacecraft - Communications -
Store-dump - Germany
SAGE - Spacecraft - Earth -
Atmosphere - USA
SAINT - Spacecraft - Military -
ASAT - USA
Saley - Yevgeni Vladimirovich Saley - Russian Cosmonaut - 1976 Air Force Group
Salto di Quirra - Launch Site - Italy
Salyut 1 - Spacecraft - Manned -
Space Station - Russia
Salyut 4 - Spacecraft - Manned -
Space Station - Russia
Salyut 6 - Spacecraft - Manned -
Space Station - Russia
Salyut 7 - Spacecraft - Manned -
Space Station - Russia
Salyut - Space Project - Manned - Spacecraft
Samolyot 5 - Spacecraft - Manned -
Rocketplane - USSR
Samos - Spacecraft - Surveillance -
Military - USA
SAMPEX - Spacecraft - Earth -
Magnetosphere - United States
San Marco - Spacecraft - Earth -
Atmosphere - Italy
San Marco - Launch Site - Kenya
Sandal; SS-4; 8K63; R-12; 63; 11K63 - Rocket Stage - Ukraine - Nitric acid/Kerosene - 39,515 kg - See Kosmos A-1
Sandal - Launch Vehicle - Ukraine - See Kosmos 11K63
Sanger II-1 - Rocket Stage - Germany - Air/LH2 - 254,000 kg
Sanger II-2 - Rocket Stage - Germany - Lox/LH2 - 112,000 kg
Sanger Sled - Rocket Stage - Germany - Lox/Alcohol - 34,000 kg
Sanger-Bredt Sled - Rocket Engine - Germany - Lox/Alcohol propellants - 116,666 kgf
Sanger-Bredt - Rocket Engine - Germany - Lox/Kerosene propellants - 145,700 kgf
Sanger-Bredt - Rocket Stage - Germany - Lox/Kerosene - 99,773 kg
Santonico - Stefano Santonico - Italian Cosmonaut - 1990 ASI Group
Sapwood - Launch Vehicle - Russia - See Vostok 8K72
SARA - Spacecraft - Astronomy -
Radio - France
Sarafanov - Gennadi Vassilyevich Sarafanov - Russian Cosmonaut - 1965 Air Force Group
SARV Retro MK I - Rocket Engine - USA - Solid propellants - 342 kgf - See Star 10
SARV Retro, MK IV - Rocket Engine - USA - Solid propellants - 567 kgf - See Star 12
SAS - Spacecraft - Solar -
- Italy
Sasin - Launch Vehicle - Russia - See R-9
SASSTO - Launch Vehicle - USA
SASSTO - Rocket Stage - USA - Lox/LH2 - 91,687 kg
Satélite de Aplicaciones Científicas - Spacecraft - Solar-
- Argentina - See SAC-B
Satan - Launch Vehicle - Ukraine - See Dnepr
Satcom - Space Project - Communications -
Satelite de Aplicaciones/Cientifico-A - Spacecraft - Technology-
- Argentina - See SAC-A
Satelite de Coleta de Dados - Spacecraft - Technology-
- Brazil - See SCD
Satellite Italiano Ricerca Industriale Orientata - Spacecraft - Technology-
Communications - Italy - See Sirio
Satellite Launch Vehicle - Launch Vehicle - India - See SLV
Satellite Launch Vehicle - Rocket Stage - India - Solid - 10,800 kg - See SLV-1
Satellite Probatoire d'Observation de la Terre - Spacecraft - Earth-
Landsat - France - See SPOT-5A-5B
Sattarov - Nail Sharipovich Sattarov - Russian Cosmonaut - 1979 Buran Group
Saturn 3S-2 - Rocket Stage - USA - Solid - 561,100 kg
Saturn A-1 - Launch Vehicle - USA
Saturn A-2 - Launch Vehicle - USA
Saturn Application Single Stage to Orbit - Launch Vehicle - USA - See SASSTO
Saturn Applications Single Stage to Orbit - Rocket Stage - USA - Lox/LH2 - 91,687 kg - See SASSTO
Saturn B-1 - Launch Vehicle - USA
Saturn C-1 - Launch Vehicle - USA - See Saturn I
Saturn C-2 - Launch Vehicle - USA
Saturn C-3B - Launch Vehicle - USA
Saturn C-3BN - Launch Vehicle - USA
Saturn C-3 - Launch Vehicle - USA
Saturn C-4B - Launch Vehicle - USA
Saturn C-4 - Launch Vehicle - USA
Saturn C-5 - Launch Vehicle - USA
Saturn C-5N - Launch Vehicle - USA
Saturn C-8 - Launch Vehicle - USA
Saturn C - Launch Vehicle Family
Saturn I RIFT - Launch Vehicle - USA
Saturn IB-11 - Rocket Stage - USA - Lox/Kerosene - 505,953 kg
Saturn IB-15 - Rocket Stage - USA - Lox/Kerosene - 478,103 kg
Saturn IB-A - Launch Vehicle - USA
Saturn IB-B - Launch Vehicle - USA
Saturn IB-CE - Launch Vehicle - USA
Saturn IB-C - Launch Vehicle - USA
Saturn IB-D - Launch Vehicle - USA
Saturn IB - Launch Vehicle - USA
Saturn IB - Rocket Stage - USA - Lox/Kerosene - 448,648 kg
Saturn IC C-3B - Rocket Stage - USA - Lox/Kerosene - 1,160,787 kg
Saturn IC C-4B - Rocket Stage - USA - Lox/Kerosene - 1,450,984 kg
Saturn IC C-5A - Rocket Stage - USA - Lox/Kerosene - 2,217,285 kg
Saturn IC-Flat Bulkhead - Rocket Stage - USA - Lox/Kerosene - 2,278,800 kg
Saturn IC - Rocket Stage - USA - Lox/Kerosene - 2,286,217 kg
Saturn II C-5A - Rocket Stage - USA - Lox/LH2 - 384,057 kg
Saturn II Stage Wet Workshop - Spacecraft - Manned -
Space Station - USA
Saturn II-INT-17 - Rocket Stage - USA - Lox/LH2 - 495,000 kg
Saturn II-SL - Rocket Stage - USA - Lox/LH2 - 490,952 kg
Saturn II - Launch Vehicle Family
Saturn II - Rocket Stage - USA - Lox/LH2 - 490,778 kg
Saturn I - Launch Vehicle Family
Saturn I - Launch Vehicle - USA
Saturn INT-05A - Launch Vehicle - USA
Saturn INT-05 - Launch Vehicle - USA
Saturn INT-11 - Launch Vehicle - USA
Saturn INT-12 - Launch Vehicle - USA
Saturn INT-13 - Launch Vehicle - USA
Saturn INT-14 - Launch Vehicle - USA
Saturn INT-15 - Launch Vehicle - USA
Saturn INT-16 - Launch Vehicle - USA
Saturn INT-17 - Launch Vehicle - USA
Saturn INT-18 - Launch Vehicle - USA
Saturn INT-19 - Launch Vehicle - USA
Saturn INT-20 - Launch Vehicle - USA
Saturn INT-21 - Launch Vehicle - USA
Saturn INT-27 - Launch Vehicle - USA
Saturn I - Rocket Stage - USA - Lox/Kerosene - 432,681 kg
Saturn IVB (S-IB) - Rocket Stage - USA - Lox/LH2 - 118,800 kg
Saturn IVB (S-V) - Rocket Stage - USA - Lox/LH2 - 119,900 kg
Saturn IVB C-3B - Rocket Stage - USA - Lox/LH2 - 52,144 kg
Saturn IVB C-5A - Rocket Stage - USA - Lox/LH2 - 102,249 kg
Saturn IVB-A - Rocket Stage - USA - Lox/LH2 - 118,800 kg
Saturn IVB - Rocket Stage - USA - Lox/LH2 - 119,920 kg
Saturn IV - Rocket Stage - USA - Lox/LH2 - 50,576 kg
Saturn LCB-Alumizine-140 - Launch Vehicle - USA
Saturn LCB-Alumizine-140 - Rocket Stage - USA - N2O4/Alumizine - 1,542,200 kg
Saturn LCB-Alumizine-250 - Launch Vehicle - USA
Saturn LCB-Alumizine-250 - Rocket Stage - USA - N2O4/Alumizine - 1,270,100 kg
Saturn LCB-Lox/RP-1 - Launch Vehicle - USA
Saturn LCB-Lox/RP-1 - Rocket Stage - USA - Lox/Kerosene - 1,360,800 kg
Saturn LCB-SR - Launch Vehicle - USA
Saturn LCB-SR - Rocket Stage - USA - Solid - 1,678,300 kg
Saturn LCB-Storable-140 - Launch Vehicle - USA
Saturn LCB-Storable-140 - Rocket Stage - USA - N2O4/UDMH - 1,995,800 kg
Saturn LCB-Storable-250 - Launch Vehicle - USA
Saturn LCB-Storable-250 - Rocket Stage - USA - N2O4/UDMH - 1,451,500 kg
Saturn MLV 5-23L-0 - Rocket Stage - USA - Lox/Kerosene - 1,180,000 kg
Saturn MLV-V-1/J-2T/200K - Launch Vehicle - USA
Saturn MLV-V-1/J-2T/250K - Launch Vehicle - USA
Saturn MLV-V-1A - Launch Vehicle - USA
Saturn MLV-V-1 - Launch Vehicle - USA
Saturn MLV-V-2 - Launch Vehicle - USA
Saturn MLV-V-3 - Launch Vehicle - USA
Saturn MLV-V-4(S)-A - Launch Vehicle - USA
Saturn MLV-V-4(S)-B - Launch Vehicle - USA
Saturn MLV-V-4(S) - Launch Vehicle - USA
Saturn MS-IC-1A - Rocket Stage - USA - Lox/Kerosene - 2,694,700 kg
Saturn MS-IC-1 - Rocket Stage - USA - Lox/Kerosene - 2,694,703 kg
Saturn MS-IC-23(L) - Rocket Stage - USA - Lox/Kerosene - 2,694,000 kg
Saturn MS-IC-25(S) - Rocket Stage - USA - Lox/Kerosene - 3,223,800 kg
Saturn MS-IC-3B - Rocket Stage - USA - Lox/Kerosene - 2,718,800 kg
Saturn MS-IC-4(S)B - Rocket Stage - USA - Lox/Kerosene - 2,875,500 kg
Saturn MS-IC/260 - Rocket Stage - USA - Lox/Kerosene - 2,721,600 kg
Saturn MS-II-1-J-2T-200K - Rocket Stage - USA - Lox/LH2 - 521,447 kg
Saturn MS-II-1-J-2T-250K - Rocket Stage - USA - Lox/LH2 - 521,447 kg
Saturn MS-II-1A - Rocket Stage - USA - Lox/LH2 - 600,800 kg
Saturn MS-II-1 - Rocket Stage - USA - Lox/LH2 - 521,447 kg
Saturn MS-II-2 - Rocket Stage - USA - Lox/LH2 - 600,788 kg
Saturn MS-II-3B - Rocket Stage - USA - Lox/LH2 - 643,200 kg
Saturn MS-II-4(S)B - Rocket Stage - USA - Lox/LH2 - 494,100 kg
Saturn MS-IVB-1A - Rocket Stage - USA - Lox/LH2 - 179,200 kg
Saturn MS-IVB-1 - Rocket Stage - USA - Lox/LH2 - 120,500 kg
Saturn MS-IVB-2 - Rocket Stage - USA - Lox/LH2 - 176,600 kg
Saturn MS-IVB-3B - Rocket Stage - USA - Lox/LH2 - 179,200 kg
Saturn MS-IVB-4(S)B - Rocket Stage - USA - Lox/LH2 - 118,400 kg
Saturn MS-IVB-x - Rocket Stage - USA - Lox/LH2 - 195,000 kg
Saturn MS-LRB-23(L) - Rocket Stage - USA - Lox/Kerosene - 874,100 kg
Saturn PFL - Rocket Stage - USA - N2O4/UDMH - 2,057,400 kg
Saturn S-1B-4 H-1 - Rocket Stage - USA - Lox/Kerosene - 444,700 kg
Saturn S-IB-2 - Rocket Stage - USA - Lox/Kerosene - 725,491 kg
Saturn S-IB-4 - Rocket Stage - USA - Lox/Kerosene - 1,813,729 kg
Saturn S-IB-A - Rocket Stage - USA - Lox/Kerosene - 448,600 kg
Saturn S-IC-8 - Rocket Stage - USA - Lox/Kerosene - 3,627,500 kg
Saturn S-IC-TLB - Launch Vehicle - USA
Saturn S-IC-TLB - Rocket Stage - USA - Lox/Kerosene - 952,500 kg
Saturn S-ID Booster - Rocket Stage - USA - Lox/Kerosene - 67,100 kg
Saturn S-ID Sustainer-1 - Rocket Stage - USA - Lox/Kerosene - 2,627,600 kg
Saturn S-ID Sustainer - Rocket Stage - USA - Lox/Kerosene - 2,219,100 kg
Saturn S-II-4 - Rocket Stage - USA - Lox/LH2 - 294,731 kg
Saturn S-II-8 - Rocket Stage - USA - Lox/LH2 - 770,835 kg
Saturn S-II-C3 - Rocket Stage - USA - Lox/LH2 - 204,044 kg
Saturn S-II - Rocket Stage - USA - Lox/LH2 - 100,000 kg
Saturn S-IVC - Rocket Stage - USA - Lox/LH2 - 204,044 kg
Saturn S-N C-3BN - Rocket Stage - USA - Nuclear/LH2 - 32,470 kg
Saturn S-N C-5N - Rocket Stage - USA - Nuclear/LH2 - 53,694 kg
Saturn S-N V-25(S)U - Rocket Stage - USA - Nuclear/LH2 - 245,760 kg
Saturn Shuttle - Launch Vehicle - USA
Saturn V Rotating Stations - Spacecraft - Manned -
Space Station - USA
Saturn V-23(L) - Launch Vehicle - USA
Saturn V-24(L) - Launch Vehicle - USA
Saturn V-25(S)B - Launch Vehicle - USA
Saturn V-25(S)U - Launch Vehicle - USA
Saturn V-3B - Launch Vehicle - USA
Saturn V-4X(U) - Launch Vehicle - USA
Saturn V-A - Launch Vehicle - USA
Saturn V-B - Launch Vehicle - USA
Saturn V-Centaur - Launch Vehicle - USA
Saturn V-C - Launch Vehicle - USA
Saturn V-D - Launch Vehicle - USA
Saturn V-ELV - Launch Vehicle - USA
Saturn V/4-260 - Launch Vehicle - USA
Saturn V - Launch Vehicle Family
Saturn V - Launch Vehicle - USA
SAVER - Spacecraft - Manned -
Bailout - USA
Savinykh - Viktor Petrovich Savinykh - Russian Cosmonaut - 1978 Civilian Engineer Group
Savitskaya - Svetlana Yevgenyevna Savitskaya - Russian Cosmonaut - 1980 Female Group
SAX - Spacecraft - Astronomy -
X-ray - Italy
Sazonov - G Sazonov - Russian Cosmonaut candidate - 1990 Journalist Group (Candidate)
SB-735 - Rocket Engine - Japan - Solid propellants - 33,430 kgf
SB-735 - Rocket Stage - Japan - Solid - 5,100 kg - See Mu-3S-0
SBS - Space Project - Communications -
Scarp - Launch Vehicle - - See R-36
SCATHA - Spacecraft - Technology -
Communications - United States
SCD - Spacecraft - Technology -
- Brazil
Schenker - Eran Schenker - Astronaut candidate - Payload Specialist (Candidate)
Schirra - Walter Marty (Wally) Schirra Jr - American Astronaut - 1959 NASA Group
Schlegel - Hans Wilhelm Schlegel - German Astronaut - 1998 ESA Group
Schlein - Paul Schlein - American Astronaut - 1979 DoD Group 1
Schmiedl - Launch Vehicle - Austria
Schmitt - Dr Harrison Hagan (Jack) Schmitt - American Astronaut - 1965 NASA Group
Schroder - Thomas Schroder - Astronaut candidate - Payload Specialist (Candidate)
Schweickart - Russel Luis (Rusty) Schweickart - American Astronaut - 1963 NASA Group
Schweikhard - William George Schweikhard - Astronaut candidate - 1962 NASA Group (Candidate)
Schwenn - Rainer Schwenn - Astronaut candidate - Payload Specialist (Candidate)
Science and Applications Manned Space Platform - Spacecraft - -
- USA
Scobee - Francis Richard Scobee - American Astronaut - 1978 NASA Group
Score - Spacecraft - Technology -
Communications - USA
Scott Russell - Russell James Scott - Astronaut candidate - 1963 NASA Group (Candidate)
Scott Winston - Winston Elliott Scott - American Astronaut - 1992 NASA Group
Scott - David Randolph (Dave) Scott - American Astronaut - 1963 NASA Group
Scout A-1 - Launch Vehicle - USA
Scout A - Launch Vehicle - USA
Scout B - Launch Vehicle - USA
Scout D - Launch Vehicle - USA
Scout F - Launch Vehicle - USA
Scout G - Launch Vehicle - USA
Scout X-1 - Launch Vehicle - USA
Scout X-2 - Launch Vehicle - USA
Scout X-3 - Launch Vehicle - USA
Scout X-4 - Launch Vehicle - USA
Scout - Launch Vehicle Family
Scrag - Launch Vehicle - Russia - See GR-1
Scramjet Test - Spacecraft - Technology -
Scramjet - USA
Scramjet - Rocket Engine - USA - Air/Slush LH2 propellants - 140,000 kgf
Scud C - Launch Vehicle - Russia - See R-17
Scud - Launch Vehicle - Russia - See R-11
Scully-Power - Paul Desmond Scully-Power - American Astronaut - Payload Specialist
Scunner - Launch Vehicle - Russia - See R-1
SDI - Spacecraft - Military -
SDI - USA
SDS-2 - Spacecraft - Communications -
Military - USA
SDS-C - Spacecraft - Communications-
Military - USA - See CAPRICORN
SDS - Spacecraft - Communications -
Military - USA
SE-1, 1-1, -2, and -4 Series - Rocket Engine - - N2O4/UDMH propellants - kgf
SE-10 - Rocket Engine - - N2O4/Aerozine-50 propellants - 4,760 kgf
SE-1 - Rocket Engine - - N2O4/UDMH propellants - kgf - See SE-1, 1-1, -2, and -4 Series
SE-5-2/-3 - Rocket Engine - - N2O4/UDMH propellants - 21 kgf
SE-5-2 - Rocket Engine - - N2O4/UDMH propellants - 21 kgf - See SE-5-2/-3
SE-6 - Rocket Engine - - N2O4/MMH propellants - 11 kgf - See SE-6
SE-7-100 - Rocket Engine - - Lox/Kerosene propellants - 45 kgf
SE-7-1 - Rocket Engine - - N2O4/MMH propellants - 32 kgf - See SE-7-1
SE-7-25 - Rocket Engine - - Lox/Kerosene propellants - 11 kgf
SE-7-85 - Rocket Engine - - Lox/Kerosene propellants - 38 kgf
SE-7 - Rocket Engine - - Lox/Kerosene propellants - 38 kgf - See SE-7-85
SE-8 - Rocket Engine - - N2O4/MMH propellants - 42 kgf - See SE-8
SE-9-3 - Rocket Engine - - N2O4/Aerozine-50 propellants - 11 kgf
SE-9-5 - Rocket Engine - - N2O4/Aerozine-50 propellants - 20 kgf
SE-9 - Rocket Engine - - N2O4/Aerozine-50 propellants - 11 kgf - See SE-9-3
Sea Bee - Launch Vehicle - USA
Sea Dragon-1 - Rocket Stage - USA - Lox/Kerosene - 11,600,000 kg
Sea Dragon-2 - Rocket Stage - USA - Lox/LH2 - 5,900,000 kg
Sea Dragon - Launch Vehicle - USA
Sea Horse-1 - Rocket Stage - USA - Lox/Kerosene - 40,000 kg
Sea Horse-2 - Rocket Stage - USA - Lox/LH2 - 15,000 kg
Sea Horse - Launch Vehicle - USA
Sea Launch - Launch Site - USA
SEALAR - Launch Vehicle - USA
Search - Article: Search the Encyclpedia Astronautica...
Searfoss - Richard Alan (Rick) Searfoss - American Astronaut - 1990 NASA Group
Seasat - Spacecraft - Earth -
Radarsat - United States
SeaStar; SeaWiFS - Spacecraft - Surveillance-
Civilian - United States - See Orbview-2
SECOR - Spacecraft - Earth -
Geodetic - USA
Secrets, Soviet - Article: James Oberg lists those secrets remaining to be disclosed...
SECS/OTS - Spacecraft - Communications -
Military - UK
SECS - Spacecraft - Communications -
Military Store-dump - United States
Seddon - Dr Margaret Rhea Seddon - American Astronaut - 1978 NASA Group
SEDSAT - Spacecraft - Technology -
- USA
SEDS - Spacecraft - Technology -
Tether - USA
See - Elliott McKay See Jr - American Astronaut - 1962 NASA Group
Sefchek - Paul Andrew Sefchek - American Astronaut - 1979 DoD Group 1
Sega - Dr Ronald Michael (Ron) Sega - American Astronaut - 1990 NASA Group
Sego - Launch Vehicle - Russia - See UR-100
Sellers - Piers John Sellers - American Astronaut - 1996 NASA Group
Semyorka - Launch Vehicle - Russia - See R-7A 8K74
Sengespeik - Dietmar Albert Fritz Sengespeik - Astronaut candidate - Payload Specialist (Candidate)
Senior - Rocket Engine - USA - Solid propellants - 48,022 kgf - See Algol 1
Senior - Rocket Stage - USA - Solid - 10,705 kg - See Algol 1
Senkevich - Dr Yuri Aleksandrovich Senkevich - Russian Cosmonaut - 1965 Physician Group
Senkov - Yu N Senkov - Russian Cosmonaut candidate - 1965 Physician Group (Candidate)
Serebrov - Aleksandr Aleksandrovich Serebrov - Russian Cosmonaut - 1978 Civilian Engineer Group
Sereda - Sereda - Russian Cosmonaut candidate - 1965 Air Force Group (Candidate)
Sergeant - Rocket Engine - USA - Solid propellants - 680 kgf
Sergeant - Rocket Stage - USA - Solid - 42 kg
SERT - Spacecraft - Technology -
Ion engine - USA
SESP - Spacecraft - Technology -
Military - USA
Sevastyanov - Vitali Ivanovich Sevastyanov - Russian Cosmonaut - 1967 Civilian Engineer Group Supplemental
Sever - Spacecraft - Manned -
Spacecraft - USSR
Severin - Sergei Gayevich Severin - Russian Cosmonaut - 1990 Civilian Engineer Group
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Last update 3 May 2001.
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© Mark Wade, 2001 .