- liquid rocket oxidizer system
- система жидкого ракетного окислителя
English-Russian glossary on space technology. 2015.
liquid rocket oxidizer system
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Liquid rocket — A liquid rocket is a rocket with an engine that uses propellants in liquid form. Liquids are desirable because their reasonably high density allows the volume and hence the mass of the tanks to be relatively low, resulting in a high mass ratio.… … Wikipedia
Rocket — This article is about vehicles powered by rocket engines. For other uses, see Rocket (disambiguation). A Soyuz U, at Baikonur Site 1/5 A rocket is a missile, spacecraft, aircraft or other vehicle which obtains thrust from a rocket engi … Wikipedia
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Liquid Propellants in Various Flight Vehicles, Table — ▪ Table rocket oxidizer fuel German V 2 liquid oxygen ethyl alcohol water (75% 25%) Atlas ICBM liquid oxygen RP 1 (kerosene) Delta First stage liquid oxygen RP 1 (kerosene) Second stage nitrogen tetroxide hydrazine UDMH* (50% 50%) Saturn First… … Universalium
Rocket Racing League — Type Private Industry Air racing · Sports · Entertainment Aerospace engineering Founded 2005 Headquarters New York, Bost … 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
Liquid air cycle engine — A liquid air cycle engine (LACE) is a spacecraft propulsion engine that attempts to gain efficiency by gathering part of its oxidizer from the atmosphere. In a LOX/LH2 bipropellant rocket the liquid oxygen needed for combustion is the majority of … Wikipedia
Hybrid rocket — A hybrid rocket propulsion system comprises propellants of two different states of matter, the most common configuration being a rocket engine composed of a solid propellant lining a combustion chamber into which a liquid or gaseous propellant is … Wikipedia
Staged combustion cycle (rocket) — Staged combustion rocket cycle. Usually, all of the fuel and a portion of the oxidizer are fed through the pre burner (fuel rich) to power the pumps. An oxygen rich circuit is possible also, but less common because of the metallurgy required. The … Wikipedia
Titan (rocket family) — Infobox Aircraft name=Titan family caption=The Titan rocket family. type=Expendable launch system with various applications manufacturer=Glenn L. Martin Company designer= first flight=1958 12 20 [cite web url=http://www.geocities.com/titan 1… … Wikipedia
Proton rocket — Infobox rocket caption =Launch of a Proton rocket name = Proton 8K82K function = Unmanned Launch Vehicle manufacturer = Khrunichev country origin = Soviet Union, Russia height = 53 m alt height = diameter = 7.4 m alt diameter = mass = 693,810 kg… … Wikipedia
