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earth-storable propellant

См. также в других словарях:

  • Rocket propellant — is mass that is stored, usually in some form of propellant tank, prior to being used as the propulsive mass that is ejected from a rocket engine in the form of a fluid jet to produce thrust.Chemical rocket propellants are most commonly used,… …   Wikipedia

  • Ariane 5 — Launching/Ariane|type=rocket Infobox rocket caption = Ariane 5 mock up name = Ariane 5 function = Heavy launch vehicle manufacturer = EADS Astrium for ESA and Arianespace country origin = Europe height = 59 m alt height = 193 ft diameter = 5.4 m… …   Wikipedia

  • SS-10 Scrag — UR 200 / SS X 10 SCRAGCentral Committee of the Communist Party and Council of Soviet Ministers released an initiative that called for the creation of a Fractional Orbital Bombardment System (FOBS) capable of sending a nuclear warhead into a 150… …   Wikipedia

  • Proton (rocket) — Proton 8K82K Launch of a Proton rocket Function Unmanned launch vehicle Manufacturer Khrunichev Country of origin Soviet Union; Russia Size Height …   Wikipedia

  • rocket and missile system — ▪ weapons system Introduction       any of a variety of weapons systems that deliver explosive warheads to their targets by means of rocket propulsion.       Rocket is a general term used broadly to describe a variety of jet propelled missiles… …   Universalium

  • Bipropellant rocket — A bipropellant rocket engine is a rocket engine that uses two propellants (very often liquid propellants) which are kept separately prior to reacting to form a hot gas to be used for propulsion.In contrast, most solid rockets have single solid… …   Wikipedia

  • Orion (Constellation program) — For deep space spacecraft based on the Orion design, see Multi Purpose Crew Vehicle. For initial design of the Orion Crew Exploration Vehicle, see Crew Exploration Vehicle. For the nuclear powered spacecraft designed in the 1950s, see Project… …   Wikipedia

  • Solar thermal rocket — Solar thermal propulsion is a form of spacecraft propulsion that makes use of solar power to directly heat reaction mass, and therefore does not require an electrical generator as most other forms of solar powered propulsion do. A solar thermal… …   Wikipedia

  • 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.Infobox rocket name = Titan II caption = Launch of a Titan II ICBM from underground silo… …   Wikipedia

  • Nitrous oxide — N2O redirects here. For other uses, see N2O (disambiguation). Laughing gas redirects here. For other uses, see Laughing gas (disambiguation). Not to be confused with nitric oxide (formula NO) or nitrogen dioxide (formula NO2). For other uses, see …   Wikipedia

  • Titan IV — infobox rocket caption = Launch of a Titan IVB launch vehicle. (USAF)name = Titan IV function = Heavy expendable launch system manufacturer = Lockheed Martin country origin = United Statescpl = $432 million (USD) cpl year = 1999height = 44m alt… …   Wikipedia

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