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201 relations: A.M. Isayev Chemical Engineering Design Bureau, Able (rocket stage), Aerozine 50, AJ10, Aleksandr Ryabenko (general), Angara (rocket family), Ariane 1, Ariane 3, Ariane 4, Atlas-Agena, Automated Transfer Vehicle, Azane, Baikonur Cosmodrome, Big dumb booster, C-Stoff, California Proposition 65 list of chemicals, Chemical Automatics Design Bureau, Chinese space program, Comparison of orbital rocket engines, Cora (rocket), Corona (satellite), Cyclone-4M, Daminozide, Delta-K, Devil's venom, DF-4, Diamant, Diamondback (missile), Diethylenetriamine, Dimethylamine, Dimethylaminopropylamine, Dimethylhydrazine, Dithiobiuret, Dnepr (rocket), Europa (rocket), Feng Bao 1, Fire, Flammability limit, Fregat, Geosynchronous Satellite Launch Vehicle, Geosynchronous Satellite Launch Vehicle Mark III, Glossary of chemical formulas, GSAT-4, Highly hazardous chemical, HN3 (nitrogen mustard), Hungnam, Hwasong-10, Hwasong-12, Hwasong-14, Hwasong-15, ..., Hydrazine, Hydrogen vehicle, Hydyne, Hypergolic propellant, Indian Space Research Organisation, Juche, Jupiter-C, Kosmos-1, Kosmos-3, Kosmos-3M, KTDU-35, KTDU-80, LGM-25C Titan II, Liquid apogee engine, Liquid rocket propellant, Liquid-propellant rocket, List of cigarette smoke carcinogens, List of IARC Group 2B carcinogens, List of Metal Gear characters, List of water-miscible solvents, Long March (rocket family), Long March 1, Long March 1D, Long March 2C, Long March 2D, Long March 2E, Long March 2F, Long March 3, Long March 3A, Long March 3B, Long March 3C, Long March 4B, Long March 4C, Long March 5, Long March 6, Long March 7, LR-87, Mars 1M, Mary Sherman Morgan, Mercury-Redstone Launch Vehicle, Methylhydrazines, MIM-3 Nike Ajax, Monomethylhydrazine, N-II (rocket), N-Nitrosodimethylamine, N1 (rocket), National Emissions Standards for Hazardous Air Pollutants, Nedelin catastrophe, Nitrosamine, NPO Energomash, Operation Behemoth, PGM-11 Redstone, Polar Satellite Launch Vehicle, Progress (spacecraft), Project Nike, Propellant, Proton (rocket family), Proton-K, Proton-M, Proton-PM, PSLV-C2, PSLV-C3, PSLV-C4, R-12 Dvina, R-14 Chusovaya, R-16 (missile), R-17 Elbrus, R-27 Zyb, R-36 (missile), Raptor (rocket engine family), RD-0210, RD-0214, RD-0216, RD-0233, RD-0236, RD-0237, RD-0243, RD-0255, RD-119, RD-215, RD-250, RD-253, RD-263, RD-270, RD-843, RD-855, RD-856, RD-861, RD-864, RM-81 Agena, Rocket propellant, Rokot, S5.142, S5.80, S5.92, S5.98M, Salyut 6, Saphir (rocket), Scramjet, Scud, Shavit, Simorgh (rocket), Soviet submarine K-219, Soyuz 29, Soyuz at the Guiana Space Centre, Soyuz-2, Soyuz-FG, Soyuz-U, Space industry of Russia, SS Metallurg Anosov, Staged combustion cycle, Strela (rocket), TATB, Thor-Able, Thor-Ablestar, Titan (rocket family), Titan IIIB, Tobacco smoke, Tonka (fuel), Triethylamine, Triisopropylamine, Trimethylamine, Tris(2-aminoethyl)amine, Tsyklon, Tsyklon-2, Tsyklon-3, Tsyklon-4, UH 25, Unha, UR-200, Valentin Glushko, Vanguard (rocket), Vega (rocket), Vikas (rocket engine), Viking (rocket engine), Vinylon, Vladimir Chelomey, White fuming nitric acid, XLR81, Yantar-2K, YF-1, YF-20, YF-23 (rocket engine), YF-40, Yuanzheng-1, Zenit (rocket family), Zenit-3F, Zvezda (ISS module), 1,2-Dimethylhydrazine, 11D428, 3MV. Expand index (151 more) »
A.M. Isayev Chemical Engineering Design Bureau
The A.M. Isayev Chemical Engineering Design Bureau (Russian: Конструкторское бюро химического машиностроения имени A.M. Исаева), also known as KB KhimMash or just KBKhM, is a Russian rocket engine design and manufacturing company.
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Able (rocket stage)
Able rocket stage, is the second stage in the Vanguard rocket cutaway view Able rocket stage engine in the foreground Able rocket stage was a rocket stage manufactured in the United States by Aerojet for the Vanguard rockets used in the Vanguard project from 1957 to 1959.
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Aerozine 50
Aerozine 50 is a 50/50 mix by weight of hydrazine and unsymmetrical dimethylhydrazine (UDMH), originally developed in the late 1950s by Aerojet General Corporation as a storable, high-energy, hypergolic fuel for the Titan II ICBM rocket engines.
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AJ10
The AJ10 is a hypergolic rocket engine manufactured by Aerojet Rocketdyne (previously Aerojet).
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Aleksandr Ryabenko (general)
Aleksandr Yakovlevich Ryabenko (Александр Яковлевич Рябенко, 25 August 1915 – March 1993) was a Soviet KGB general who was responsible for personal security of Leonid Brezhnev.
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Angara (rocket family)
The Angara rocket family is a family of space-launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center.
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Ariane 1
Ariane 1 was the first rocket in the Ariane family of expendable launch systems.
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Ariane 3
Ariane 3 was a European expendable carrier rocket, which was used for eleven launches between 1984 and 1989.
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Ariane 4
The Ariane 4 was an expendable launch system, designed by the Centre national d'études spatiales while being manufactured and marketed by its subsidiary Arianespace.
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Atlas-Agena
The Atlas-Agena was an American expendable launch system derived from the SM-65 Atlas missile.
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Automated Transfer Vehicle
The Automated Transfer Vehicle, originally Ariane Transfer Vehicle or ATV, was an expendable cargo spacecraft developed by the European Space Agency (ESA).
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Azane
Azanes are acyclic, saturated hydronitrogens, which means that they consist only of hydrogen and nitrogen atoms and all bonds are single bonds.
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Baikonur Cosmodrome
Baikonur Cosmodrome (translit; translit) is a spaceport located in an area of southern Kazakhstan leased to Russia.
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Big dumb booster
Big Dumb Booster (BDB) is a general class of launch vehicle based on the premise that it is cheaper to operate large rockets of simple design than it is to operate smaller, more complex ones regardless of the lower payload efficiency.
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C-Stoff
C-Stoff ("C stuff") was a reductant used in bipropellant rocket fuels (as a fuel itself) developed by Hellmuth Walter Kommanditgesellschaft in Germany during World War II.
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California Proposition 65 list of chemicals
The following is a list of chemicals published as a requirement of Safe Drinking Water and Toxic Enforcement Act of 1986, commonly known as California Proposition 65, that are "known to the state to cause cancer or reproductive toxicity" as of December 29, 2017.
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Chemical Automatics Design Bureau
Chemical Automatics Design Bureau (CADB), also KB Khimavtomatika (Конструкторское бюро химавтоматики, КБХА, KBKhA), is a Russian design bureau founded by the NKAP (People's Commissariat of the Aircraft Industry) in 1941 and led by Semyon Kosberg until his death in 1965.
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Chinese space program
The space program of the People's Republic of China is directed by the China National Space Administration (CNSA).
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Comparison of orbital rocket engines
This page is an incomplete list of orbital rocket engine data.
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Cora (rocket)
Cora is the name of a single-stage French experimental rocket, which was propelled with nitrogen tetroxide and UDMH.
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Corona (satellite)
The Corona program was a series of American strategic reconnaissance satellites produced and operated by the Central Intelligence Agency Directorate of Science & Technology with substantial assistance from the U.S. Air Force.
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Cyclone-4M
The Cyclone-4M is a Ukrainian carrier rocket which is being developed for commercial satellite launches.
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Daminozide
Daminozide – also known as Alar, Kylar, B-NINE, DMASA, SADH, or B 995 – is a plant growth regulator, a chemical sprayed on fruit to regulate their growth, make their harvest easier, and keep apples from falling off the trees before they are ripe.
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Delta-K
The Delta-K is an American rocket stage, developed by McDonnell Douglas and Aerojet.
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Devil's venom
Devil's venom was a nickname coined by Soviet rocket scientists for a liquid rocket fuel composed of a dangerous combination of nitric acid and hydrazine—specifically, hypergolic UDMH-nitric acid.
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DF-4
The Dong Feng 4 or DF-4 (also known as the CSS-3) is a two-stage Chinese Intercontinental ballistic missile with liquid fuel (Nitric acid/Unsymmetrical dimethylhydrazine).
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Diamant
The Diamant rocket (Diamant is French for "diamond") was the first exclusively French expendable launch system and at the same time the first satellite launcher not built by either the United States or USSR.
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Diamondback (missile)
The Diamondback was a proposed nuclear-armed air-to-air missile studied by the United States Navy's Naval Ordnance Test Station during the 1950s.
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Diethylenetriamine
Diethylenetriamine (abbreviated DETA and also known as 2,2’-Iminodi(ethylamine)) is an organic compound with the formula HN(CH2CH2NH2)2.
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Dimethylamine
Dimethylamine is an organic compound with the formula (CH3)2NH.
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Dimethylaminopropylamine
Dimethylaminopropylamine (aka "DMAPA") is a diamine used in the preparation of some surfactants, such as cocamidopropyl betaine which is an ingredient in many personal care products including soaps, shampoos, and cosmetics.
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Dimethylhydrazine
Dimethylhydrazine is the name of two compounds with the molecular formula C2H8N2.
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Dithiobiuret
Dithiobiuret is an organosulfur compound with the formula HN(C(S)NH2)2.
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Dnepr (rocket)
The Dnepr rocket (translit; translit) is a space launch vehicle named after the Dnieper River.
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Europa (rocket)
The Europa rocket was an early expendable launch system of the European Launcher Development Organisation (ELDO), which was the precursor to the European Space Agency (ESA).
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Feng Bao 1
The Feng Bao 1 (Chinese: 风暴, meaning Storm), also known as FB-1, was a Chinese carrier rocket launched between 1972 and 1981.
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Fire
Fire is the rapid oxidation of a material in the exothermic chemical process of combustion, releasing heat, light, and various reaction products.
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Flammability limit
Mixtures of dispersed combustible materials (such as gaseous or vaporised fuels, and some dusts) and air will burn only if the fuel concentration lies within well-defined lower and upper bounds determined experimentally, referred to as flammability limits or explosive limits.
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Fregat
Fregat (Фрегат, frigate) is an upper stage developed by NPO Lavochkin in the 1990s, which is used in some Soyuz and Zenit rockets.
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Geosynchronous Satellite Launch Vehicle
Geosynchronous Satellite Launch Vehicle abbreviated as GSLV, is an expendable launch system operated by the Indian Space Research Organisation (ISRO).
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Geosynchronous Satellite Launch Vehicle Mark III
The Geosynchronous Satellite Launch Vehicle Mark III (GSLV-III), also referred to as the Launch Vehicle Mark 3 (LVM3) is a three-stage medium-lift launch vehicle developed by the Indian Space Research Organisation (ISRO).
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Glossary of chemical formulas
This is a list of common chemical compounds with chemical formulas and CAS numbers, indexed by formula.
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GSAT-4
GSAT-4, also known as HealthSat, was an experimental communication and navigation satellite launched in April 2010 by the Indian Space Research Organisation on the maiden flight of the Geosynchronous Satellite Launch Vehicle Mk.II rocket.
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Highly hazardous chemical
A highly hazardous chemical is a substance classified by the American Occupational Safety and Health Administration as material that is both toxic and reactive and whose potential for human injury is high if released.
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HN3 (nitrogen mustard)
Tris(2-chloroethyl)amine is the organic compound with the formula N(CH2CH2Cl)3.
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Hungnam
Hŭngnam is a district of Hamhung, the third largest city in North Korea.
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Hwasong-10
The Hwasong-10 (Chosŏn'gŭl: 화성 10호; hancha: 火星 10號), also known by the names BM-25 system and Musudan, is a mobile intermediate-range ballistic missile developed by North Korea.
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Hwasong-12
The Hwasong-12 (화성 12, meaning Mars 12; KN-17 under the U.S. naming convention) is a mobile intermediate-range ballistic missile developed by North Korea. The Hwasong-12 was first revealed to the international community in a military parade on 14 April 2017 celebrating the Day of the Sun which is the birthday anniversary of North Korea's founding President, Kim Il-sung.
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Hwasong-14
The Hwasong-14 (Chosŏn'gŭl: 화성 14호; hancha: 火星 14号, meaning Mars-14), also known under alternative US designation codename KN-20, is a mobile intercontinental ballistic missile developed by North Korea.
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Hwasong-15
The Hwasong-15 is an intercontinental ballistic missile developed by North Korea.
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Hydrazine
Hydrazine is an inorganic compound with the chemical formula (also written), called diamidogen, archaically.
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Hydrogen vehicle
A hydrogen vehicle is a vehicle that uses hydrogen as its onboard fuel for motive power.
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Hydyne
Hydyne is a mixture of 60% unsymmetrical dimethylhydrazine (UDMH) and 40% diethylenetriamine (DETA), developed in 1957 at Rocketdyne for use in liquid-fuel rockets.
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Hypergolic propellant
A hypergolic propellant combination used in a rocket engine is one whose components spontaneously ignite when they come into contact with each other.
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Indian Space Research Organisation
The Indian Space Research Organisation (ISRO) is the space agency of the Government of India headquartered in the city of Bangalore.
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Juche
Juche (subject;; usually left untranslated or translated as "self-reliance") is the official state ideology of North Korea, described by the government as Kim Il-sung's "original, brilliant and revolutionary contribution to national and international thought".
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Jupiter-C
The Jupiter-C was an American research and development vehicle developed from the Jupiter-A. Jupiter-C was used for three sub-orbital spaceflights in 1956 and 1957 to test re-entry nosecones that were later to be deployed on the more advanced PGM-19 Jupiter mobile missile.
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Kosmos-1
The Kosmos-1 (GRAU Index: 65S3, also known as Cosmos-1) was a Soviet carrier rocket (Kosmos (rocket family)), derived from the R-14 missile, which was used to orbit satellites in 1964 and 1965.
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Kosmos-3
The Kosmos-3 (GRAU Index: 11K65, also known as Cosmos-3) was a Soviet carrier rocket (Kosmos (rocket family)), derived from the R-14 missile, which was used to orbit satellites between 1966 and 1968.
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Kosmos-3M
The Kosmos-3M (Космос-3М meaning "Cosmos", GRAU index 11K65M) is a Russian space launch vehicle, member of the Kosmos (rocket family).
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KTDU-35
The KTDU-35 (GRAU Index 11D62) was a Soviet spacecraft propulsion system composed of two liquid rocket engines, the primary, S5.60 (SKD) and the secondary S5.35 (DKD), fed from the same propellant tanks.
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KTDU-80
The KTDU-80 (Russian: Корректирующе-Тормозная Двигательная Установка, КТДУ) is the latest of a family of integrated propulsion system that KB KhIMMASH has implemented for the Soyuz since the Soyuz-T. It integrates main propulsion, RCS and attitude control in a single system pressure fed from a common dual string redundant pressurized propellant system.
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LGM-25C Titan II
The Titan II was an intercontinental ballistic missile (ICBM) and space launcher developed by the Glenn L. Martin Company from the earlier Titan I missile.
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Liquid apogee engine
A liquid apogee engine (LAE), or apogee engine, refers to a type of chemical rocket engine typically used as the main engine in a spacecraft.
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Liquid rocket propellant
The highest specific impulse chemical rockets use liquid propellants (liquid-propellant rockets).
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Liquid-propellant rocket
A liquid-propellant rocket or liquid rocket is a rocket engine that uses liquid propellants.
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List of cigarette smoke carcinogens
Commercial tobacco smoke is a mixture of more than 5000 chemicals.
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List of IARC Group 2B carcinogens
Substances, mixtures and exposure circumstances in this list have been classified by the International Agency for Research on Cancer (IARC) as Group 2B: The agent (mixture) is "possibly carcinogenic to humans".
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List of Metal Gear characters
The ''Metal Gear'' franchise features a large number of characters created by Hideo Kojima and designed by Yoji Shinkawa.
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List of water-miscible solvents
The following compounds are liquid at room temperature and are completely miscible with water; they are often used as solvents.
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Long March (rocket family)
A Long March rocket or Changzheng rocket in Chinese pinyin is any rocket in a family of expendable launch systems operated by the People's Republic of China.
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Long March 1
The Long March 1 (长征一号), also known as the Changzheng-1 (CZ-1), was the first member of China's Long March rocket family.
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Long March 1D
During the 1990s CALT developed an improved version of the DF-4 to test the reentry vehicle warheads of the DF-31.
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Long March 2C
Long March 2C (LM-2C), or Chang Zheng 2C (CZ-2C) as in Chinese pinyin is a member of the Long March 2 rocket family, an expendable launch system operated by the People's Republic of China.
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Long March 2D
The Long March 2D, also known as the Chang Zheng 2D, CZ-2D and LM-2D, is a Chinese orbital carrier rocket.
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Long March 2E
The Long March 2E, also known as the Chang Zheng 2E, CZ-2E and LM-2E, was a Chinese orbital carrier rocket from the Long March 2 family.
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Long March 2F
The Long March 2F (Changzheng 2F), also known as the CZ-2F, LM-2F and Shenjian, is a Chinese orbital carrier rocket, part of the Long March 2 rocket family.
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Long March 3
The Long March 3, also known as the Changzheng 3, CZ-3 and LM-3, was a Chinese orbital carrier rocket.
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Long March 3A
The Long March 3A, also known as the Chang Zheng 3A, CZ-3A and LM-3A, is a Chinese orbital carrier rocket.
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Long March 3B
The Long March 3B (Chang Zheng 3B), also known as the CZ-3B and LM-3B, is a Chinese orbital carrier rocket. Introduced in 1996, it is launched from Launch Area 2 and 3 at the Xichang Satellite Launch Center in Sichuan. A three-stage rocket with four strap-on liquid rocket boosters, it is currently the most powerful member of the Long March rocket family and the heaviest of the Long March 3 rocket family, and is mainly used to place communications satellites into geosynchronous orbits. An enhanced version, the Long March 3B/E or G2, was introduced in 2007 to increase the rocket's GTO cargo capacity and lift heavier GEO communications satellites. The Long March 3B also served as the basis for the medium-capacity Long March 3C, which was first launched in 2008., the Long March 3B and 3B/E have conducted 43 successful launches, plus one failure and two partial failures, giving them a success rate of.
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Long March 3C
The Long March 3C, also known as the Changzheng 3C, CZ-3C and LM-3C, is a Chinese orbital carrier rocket.
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Long March 4B
The Long March 4B, also known as the Chang Zheng 4B, CZ-4B and LM-4B is a Chinese orbital carrier rocket.
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Long March 4C
The Long March 4C, also known as the Chang Zheng 4C, CZ-4C and LM-4C, previously designated Long March 4B-II, is a Chinese orbital carrier rocket.
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Long March 5
Long March 5 (LM-5, CZ-5, or Changzheng 5) is a Chinese heavy lift launch system developed by China Academy of Launch Vehicle Technology (CALT).
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Long March 6
The Long March 6 or Chang Zheng 6 as in pinyin, abbreviated LM-6 for export or CZ-6 within China, is a Chinese liquid-fuelled carrier rocket of the Long March family, which was developed by the China Aerospace Science and Technology Corporation and the Shanghai Academy of Spaceflight Technology.
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Long March 7
The Long March 7, or Chang Zheng 7 as in pinyin, abbreviated LM-7 for export or CZ-7 within China, originally Long March 2F/H or Chang Zheng 2F/H, is a Chinese liquid-fuelled carrier rocket of the Long March family, developed by the China Aerospace Science and Technology Corporation.
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LR-87
The LR87 was an American liquid-propellant rocket engine, which was used on the first stages of Titan intercontinental ballistic missiles and launch vehicles.
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Mars 1M
Mars 1M was a series of two unmanned spacecraft which were used in the first Soviet missions to explore Mars.
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Mary Sherman Morgan
Mary Sherman Morgan (November 4, 1921 – August 4, 2004) was a U.S. rocket fuel scientist credited with the invention of the liquid fuel Hydyne in 1957, which powered the Jupiter-C rocket that boosted the United States' first satellite, Explorer 1.
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Mercury-Redstone Launch Vehicle
The Mercury-Redstone Launch Vehicle, designed for NASA's Project Mercury, was the first American manned space booster.
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Methylhydrazines
Methylhydrazines are hydrazines that have additional methyl groups.
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MIM-3 Nike Ajax
The United States Army's Nike Ajax was the world's first operational surface-to-air missile (SAM), entering service in 1954.
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Monomethylhydrazine
Monomethylhydrazine (MMH) is a volatile hydrazine chemical with the chemical formula CH3(NH)NH2.
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N-II (rocket)
The N-II or N-2 was a derivative of the American Delta rocket, produced under licence in Japan.
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N-Nitrosodimethylamine
N-Nitrosodimethylamine (NDMA), also known as dimethylnitrosamine (DMN), is a semi-volatile organic chemical, produced as by-product of several industrial processes and present at very low levels in certain foodstuffs, especially those cooked, smoked, or cured.
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N1 (rocket)
The N1 (Russian: Н1, from Ракета-носитель, Raketa-Nositel, carrier) was a super heavy-lift launch vehicle intended to deliver payloads beyond low Earth orbit, acting as the Soviet counterpart to the US Saturn V. It was designed with crewed extra-orbital travel in mind.
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National Emissions Standards for Hazardous Air Pollutants
The National Emission Standards for Hazardous Air Pollutants, also using the acronym NESHAP, are emission standards set by the United States Environmental Protection Agency—EPA.
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Nedelin catastrophe
The Nedelin catastrophe or Nedelin disaster was a launch pad accident that occurred on 24 October 1960 at Baikonur test range (of which Baikonur Cosmodrome is a part), during the development of the Soviet ICBM R-16.
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Nitrosamine
Nitrosamines are chemical compounds of the chemical structure R1N(–R2)–N.
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NPO Energomash
NPO Energomash “V.
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Operation Behemoth
Operation Behemoth-1, Behemoth-2 (Бегемот - Begemot, Hippopotamus) were military exercises held by the Soviet Northern Fleet in 1989 and 1991.
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PGM-11 Redstone
The PGM-11 Redstone was the first large American ballistic missile.
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Polar Satellite Launch Vehicle
The Polar Satellite Launch Vehicle (PSLV) is an expendable launch system developed and operated by the Indian Space Research Organisation (ISRO).
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Progress (spacecraft)
The Progress (Прогресс) is a Russian expendable cargo spacecraft.
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Project Nike
Project Nike, (Greek: Νίκη, "Victory", pronounced), was a U.S. Army project, proposed in May 1945 by Bell Laboratories, to develop a line-of-sight anti-aircraft missile system.
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Propellant
A propellant or propellent is a chemical substance used in the production of energy or pressurized gas that is subsequently used to create movement of a fluid or to generate propulsion of a vehicle, projectile, or other object.
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Proton (rocket family)
Proton (Russian: Протон) (formal designation: UR-500) is an expendable launch system used for both commercial and Russian government space launches.
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Proton-K
The Proton-K, also designated Proton 8K82K after its GRAU index, 8K82K, was a Russian, previously Soviet, carrier rocket derived from the earlier Proton.
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Proton-M
The Proton-M, (Протон-М) GRAU index 8K82M or, is a Russian heavy-lift launch vehicle derived from the Soviet-developed Proton.
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Proton-PM
OJSC Proton-PM (Russian: ОАО «Протон-ПМ») is a Russian engine and heavy machinery manufacturing plant.
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PSLV-C2
PSLV-C2 was the second operational launch and overall fifth mission of the PSLV program.
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PSLV-C3
PSLV-C3 was the third operational launch and overall sixth mission of the PSLV program.
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PSLV-C4
PSLV-C4 was the fourth operational launch and overall seventh mission of the PSLV program.
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R-12 Dvina
The R-12 was a theatre ballistic missile developed and deployed by the Soviet Union during the Cold War.
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R-14 Chusovaya
The R-14 Chusovaya (Чусовая) was a single stage Intermediate-range ballistic missile developed by the Soviet Union during the Cold War.
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R-16 (missile)
The R-16 was the first successful intercontinental ballistic missile deployed by the Soviet Union.
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R-17 Elbrus
The R-17 Elbrus, GRAU index 9K72 is a tactical ballistic missile, initially developed by the Soviet Union.
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R-27 Zyb
The R-27 Zyb was a submarine-launched ballistic missile developed by the Soviet Union and employed by the Soviet Navy from 1968 through 1988.
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R-36 (missile)
The R-36 (Р-36) is a family of intercontinental ballistic missiles (ICBMs) and space launch vehicles (Tsyklon) designed by the Soviet Union during the Cold War.
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Raptor (rocket engine family)
Raptor is a family of cryogenic, methane-fueled rocket engines under development by SpaceX.
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RD-0210
The RD-0210 (GRAU Index: 8D411K) is also known as the RD-465.
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RD-0214
The RD-0214 (GRAU Index: 8D811) is a rocket vernier engine burning N2O4 and UDMH in a gas generator cycle.
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RD-0216
The RD-0216 and RD-0217 are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle.
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RD-0233
The RD-0233 (GRAU Index 15D95) and RD-0234 (GRAU Index 15D96) are liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle.
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RD-0236
The RD-0236 (GRAU Index 15D114) is a liquid rocket vernier engine, burning N2O4 and UDMH in the gas generator cycle.
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RD-0237
The RD-0237 (GRAU Index 15D114) is a pressure-fed liquid rocket vernier engine, burning N2O4 and UDMH.
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RD-0243
The RD-0243 is a propulsion module composed of an RD-0244 main engine and a RD-0245 vernier engine.
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RD-0255
The RD-0255 is a propulsion module composed of an RD-0256 main engine and a RD-0257 vernier engine.
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RD-119
The RD-119 (GRAU Index 8D710) was a liquid rocket engine, burning liquid oxygen and UDMH in the Gas Generator cycle.
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RD-215
The RD-215 (GRAU Index 8D513) was a dual nozzle liquid rocket engine, burning AK-27 (a mixture of 73% nitric acid and 27% N2O4 + iodine passivant) and UDMH.
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RD-250
The RD-250 (GRAU Index 8D518) is the base version of a dual nozzle family of liquid rocket engines, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle.
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RD-253
The RD-253 (Раке́тный дви́гатель 253, Rocket Engine 253) and its later variants, the RD-275 and RD-275M, are liquid-propellant rocket engines developed in the Soviet Union by Energomash.
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RD-263
The RD-263 (GRAU Index 15D117) is a liquid rocket engine, burning N2O4 and UDMH in the oxidizer rich staged combustion cycle.
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RD-270
RD-270 (Ра́кетный дв́игатель 270, Rocket Engine 270, 8D420) is a single-chamber liquid-bipropellant rocket engine designed by Energomash (USSR) in 1960–1970.
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RD-843
The RD-843 is a Ukrainian single nozzle liquid propellant rocket engine burning pressure-fed UDMH and nitrogen tetroxide.
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RD-855
The RD-855 (GRAU Index 8D68M), also known as the RD-68M, is a four nozzle liquid rocket vernier engine, burning N2O4 and UDMH in a gas generator cycle.
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RD-856
The RD-855 (GRAU Index 8D69M), also known as the RD-69M, is a four nozzle liquid rocket vernier engine, burning N2O4 and UDMH in a gas generator cycle.
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RD-861
The RD-861 is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle.
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RD-864
The RD-864 (GRAU: 15D177) is a Soviet liquid propellant rocket engine burning UDMH and nitrogen tetroxide in a gas generator combustion cycle.
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RM-81 Agena
The RM-81 Agena was an American rocket upper stage and satellite bus which was developed by Lockheed initially for the canceled WS-117L reconnaissance satellite program.
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Rocket propellant
Rocket propellant is a material used either directly by a rocket as the reaction mass (propulsive mass) that is ejected, typically with very high speed, from a rocket engine to produce thrust, and thus provide spacecraft propulsion, or indirectly to produce the reaction mass in a chemical reaction.
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Rokot
Rokot (Рокот meaning Rumble or Boom), also transliterated Rockot, is a Russian space launch vehicle that can launch a payload of 1,950 kilograms into a 200 kilometre Earth orbit with 63° inclination.
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S5.142
The S5.142 (AKA DST-25) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85.
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S5.80
The S5.80 is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85.
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S5.92
The S5.92 is a Russian rocket engine, currently used on the Fregat upper stage.
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S5.98M
The S5.98M, also known as the 14D30, is a Russian rocket engine, currently powering the Briz upper stages.
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Salyut 6
Salyut 6 (Салют-6; lit. Salute 6), DOS-5, was a Soviet orbital space station, the eighth flown as part of the Salyut programme.
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Saphir (rocket)
Saphir VE231 (French, meaning sapphire) was a French sounding rocket.
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Scramjet
A scramjet ("supersonic combustion ramjet") is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow.
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Scud
Scud is the name of a series of tactical ballistic missiles developed by the Soviet Union during the Cold War.
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Shavit
Shavit (Hebrew: "comet" – שביט) is a small lift launch vehicle produced by Israel from 1982 onwards, to launch satellites into orbit.
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Simorgh (rocket)
Simorgh (ماهوارهبر سیمرغ, Phoenix), also called Safir-2, is an Iranian expendable small-capacity orbital carrier rocket, which was originally scheduled to make its maiden flight in 2010.
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Soviet submarine K-219
K-219 was a Project 667A ''Navaga''-class ballistic missile submarine (NATO reporting name Yankee I) of the Soviet Navy.
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Soyuz 29
Soyuz 29 (Союз 29, Union 29) was a 1978 manned Soviet space mission to the Salyut 6 space station.
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Soyuz at the Guiana Space Centre
Soyuz at the Guiana Space Centre (also known as Soyuz at CSG or Arianespace Soyuz) is an ongoing ESA programme for operating Soyuz-ST launch vehicles from Guiana Space Centre (CSG), providing medium-size launch capability for Arianespace to accompany the light Vega and heavy-lift Ariane 5.
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Soyuz-2
Soyuz-2, GRAU index 14A14, is the collective designation for the new version of the Russian Soyuz rocket.
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Soyuz-FG
The Soyuz-FG launch vehicle is an improved version of the Soyuz-U from the R-7 family of rockets, designed and constructed by TsSKB-Progress in Samara.
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Soyuz-U
The Soyuz-U launch vehicle was an improved version of the original Soyuz rocket.
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Space industry of Russia
Space industry of Russia consists of over 100 companies and employs 250,000 people.
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SS Metallurg Anosov
The SS Metallurg Anosov (Russian: Металлург Аносов) was a merchant ship of Black Sea Shipping Company (Soviet Union).
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Staged combustion cycle
The staged combustion cycle (sometimes known as topping cycle or preburner cycle) is a power cycle of a bipropellant rocket engine.
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Strela (rocket)
Strela (Стрела, arrow) is a Russian orbital carrier rocket, derived from the Soviet/Russian UR-100NU missile.
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TATB
TATB, triaminotrinitrobenzene or 2,4,6-triamino-1,3,5- trinitrobenzene is an aromatic explosive, based on the basic six-carbon benzene ring structure with three nitro functional groups (NO2) and three amine (NH2) groups attached, alternating around the ring.
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Thor-Able
The Thor-Able was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960.
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Thor-Ablestar
The Thor-Ablestar, or Thor Able-Star, also known as Thor-Epsilon was an early American expendable launch system consisting of a PGM-17 Thor missile, with an Ablestar upper stage.
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Titan (rocket family)
Titan is a family of United States expendable rockets used between 1959 and 2005.
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Titan IIIB
Titan IIIB was the collective name for a number of derivatives of the Titan II ICBM and Titan III launch vehicle, modified by the addition of an Agena upper stage.
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Tobacco smoke
Cigarette smoke is an aerosol produced by the incomplete combustion of tobacco during the smoking of cigarettes.
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Tonka (fuel)
Tonka (also TONKA-250 and R-Stoff) is the name given to a German-designed rocket propellant first used in the Wasserfall missile; it has also more recently been used by North Korea but found its greatest applications (under the name TG-02) in the Soviet Union, for example, in the propulsion projects of the A.M. Isayev Chemical Engineering Design Bureau.
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Triethylamine
Triethylamine is the chemical compound with the formula N(CH2CH3)3, commonly abbreviated Et3N.
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Triisopropylamine
Triisopropylamine is an organic chemical compound consisting of three isopropyl groups bound to a central nitrogen atom.
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Trimethylamine
Trimethylamine (TMA) is an organic compound with the formula N(CH3)3.
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Tris(2-aminoethyl)amine
Tris(2-aminoethyl)amine is the organic compound with the formula N(CH2CH2NH2)3.
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Tsyklon
The Tsyklon (Циклон, "Cyclone", also known as Tsiklon), GRAU index 11K67, was a Soviet-designed expendable launch system, primarily used to put Cosmos satellites into low Earth orbit.
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Tsyklon-2
The Tsyklon-2 (cyclone-2), also known as Tsiklon-2 and Tsyklon-M, GRAU index 11K69, is a Ukrainian, previously Soviet orbital carrier rocket.
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Tsyklon-3
The Tsyklon-3, also known as Tsiklon-3, GRAU index 11K68, was a Soviet, and subsequently Ukrainian orbital carrier rocket.
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Tsyklon-4
The Tsyklon-4, also known as Tsiklon-4 and Cyclone-4, was a Ukrainian carrier rocket which was being developed for commercial satellite launches.
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UH 25
UH 25 is a fuel mixture for rockets.
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Unha
The Unha or Eunha (은하, 銀河, "Galaxy") is a North Korean expendable carrier rocket, which partially utilizes the same delivery system as the Taepodong-2 long-range ballistic missile.
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UR-200
The UR-200 was an intercontinental ballistic missile (ICBM) developed by OKB-52 of Vladimir Nikolaevich Chelomey in the Soviet Union.
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Valentin Glushko
Valentin Petrovich Glushko (Валенти́н Петро́вич Глушко́, Valentin Petrovich Glushko; Валентин Петрович Глушко, Valentyn Petrovych Hlushko; born 2 September 1908 – 10 January 1989), was a Soviet engineer, and designer of rocket engines during the Soviet/American Space Race.
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Vanguard (rocket)
The Vanguard rocket was intended to be the first launch vehicle the United States would use to place a satellite into orbit.
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Vega (rocket)
Vega (Vettore Europeo di Generazione Avanzata, meaning "Advanced generation European carrier rocket"), is an expendable launch system in use by Arianespace jointly developed by the Italian Space Agency and the European Space Agency.
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Vikas (rocket engine)
The Vikas (an acronym for '''''VIK'''''ram '''''A'''''mbalal '''''S'''''arabhai) is a family of liquid fuelled rocket engines conceptualized and designed by the Liquid Propulsion Systems Centre in the 1970s.
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Viking (rocket engine)
The Viking rocket engines were members of a series of bipropellant engines for the first and second stages of the Ariane 1 through Ariane 4 commercial launch vehicles, using storable, hypergolic propellants, N2O4/UH 25 (mixture 75% UDMH and 25% Hydrazine.) The earliest versions, developed in 1965, had a sea-level thrust of about 190 kN.
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Vinylon
Vinylon, also known as Vinalon, is a synthetic fiber produced from polyvinyl alcohol, using anthracite and limestone as raw materials.
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Vladimir Chelomey
Vladimir Nikolayevich Chelomey (Russian: Влади́мир Никола́евич Челоме́й; Ukrainian: Володимир Миколайович Челомей; 30 June 1914 – 8 December 1984) was a Soviet mechanics scientist, aviation and missile engineer.
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White fuming nitric acid
White fuming nitric acid (WFNA) is a storable liquid oxidizer used with kerosene and hydrazine rocket fuel.
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XLR81
The Bell Aerosystems Company XLR81 (Model 8096) was an American liquid-propellant rocket engine, which was used on the Agena upper stage.
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Yantar-2K
Yantar-2K (Янтарь meaning amber) was a type of Soviet reconnaissance satellite which supplemented and eventually replaced the Zenit spacecraft.
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YF-1
The YF-1 was a Chinese liquid rocket engine burning N2O4 and UDMH in an gas generator cycle.
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YF-20
The YF-20 is a Chinese liquid-fuel rocket engine burning N2O4 and UDMH in an gas generator cycle.
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YF-23 (rocket engine)
The YF-23 is a liquid rocket vernier engine, burning N2O4 and UDMH.
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YF-40
The YF-40 is a Chinese liquid rocket engine burning N2O4 and UDMH in an gas generator cycle.
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Yuanzheng-1
The Yuanzheng-1 (YZ-1) is a restartable rocket upper stage developed by the China Academy of Launch Vehicle Technology (CALT) used as a fourth stage to enable the Long March 3B and Long March 3C launch vehicles to deploy payloads directly to high energy orbits like medium Earth orbit (MEO) and geostationary orbit (GSO).
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Zenit (rocket family)
Zenit (Зеніт, Зени́т; meaning Zenith) is a family of space launch vehicles designed by the Yuzhnoye Design Bureau in Dnipro, Ukraine, which was then part of the Soviet Union.
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Zenit-3F
The Zenit-3F, Zenit-3SLBF or Zenit-2SB/Fregat is an expendable carrier rocket.
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Zvezda (ISS module)
Zvezda (Звезда́, meaning "star"), DOS-8, also known as the Zvezda Service Module, is a component of the International Space Station (ISS).
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1,2-Dimethylhydrazine
1,2-Dimethylhydrazine, or symmetrical dimethylhydrazine, is the organic compound with the formula (CH3NH)2.
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11D428
The 11D428A-16 (manufacturer's name RDMT-135M) is a liquid pressure-fed rocket engine burning N2O4/UDMH with an O/F of 1.85.
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3MV
The 3MV planetary probe (short for 3rd generation Mars-Venus) is a designation for a common design used by early Soviet unmanned probes to Mars and Venus.
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Redirects here:
1,1-Dimethylhydrazine, 1,1-dimethylhydrazine, Dimazine, UDMH, Uns-dimethylhydrazine, Unsymmetrical Dimethyl Hydrazine, Unsymmetrical dimethyl hydrazine.
References
[1] https://en.wikipedia.org/wiki/Unsymmetrical_dimethylhydrazine
