- storable-liquid propellant rocket engine
- ЖРД под топливо длительного хранения
English-russian astronautics dictionary. - M.: Military Publishing house. Compiled by F. P. Suprun, K. V. Shirokov. 1964.
English-russian astronautics dictionary. - M.: Military Publishing house. Compiled by F. P. Suprun, K. V. Shirokov. 1964.
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
Liquid rocket propellants — The highest specific impulse chemical rockets use liquid propellants. This type of propellent has a long history going back to the first rockets and is still in use in for example the Space Shuttle and Ariane 5. History Early developmentOn March… … Wikipedia
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
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
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
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
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
NPO Energomash — Model of the RD 170 Engine developed by NPO Energomash. NPO Energomash “V. P. Glushko” is a Russian manufacturer originated from design bureau, which focuses primarily on the development and production of liquid propellant rocket engines. NPO… … Wikipedia
R-12 (missile) — Infobox Weapon is missile=yes name=R 12 caption= origin= type=Medium range ballistic missile used by= manufacturer=Yuzhmash unit cost=unknown propellant= production date= service=4 March 1959 engine=liquid rocket motor, 3 stages engine power=… … Wikipedia
Nitrous oxide fuel blend — propellants are a class of liquid rocket propellants. The fuel and oxidizer are blended and stored, and are sometimes referred to as mixed monopropellants . Upon use, the propellant is heated or passed over a catalyst bed and the Nitrous oxide… … 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