- hypergolic bipropellant
- hipergol paliwo rakietowe
English-Polish dictionary for engineers. 2013.
English-Polish dictionary for engineers. 2013.
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
Rocket engine — RS 68 being tested at NASA s Stennis Space Center. The nearly transparent exhaust is due to this engine s exhaust being mostly superheated steam (water vapor from its propellants, hydrogen and oxygen) … Wikipedia
Mars Observer — Artist rendering of Mars Observer in orbit around Mars. Operator NASA / JPL … Wikipedia
Monomethylhydrazine — Monomethylhydrazine … Wikipedia
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
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
Spacecraft propulsion — A remote camera captures a close up view of a Space Shuttle Main Engine during a test firing at the John C. Stennis Space Center in Hancock County, Mississippi Spacecraft propulsion is any method used to accelerate spacecraft and artificial… … 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
Dinitrogen tetroxide — IUPAC name Dinitrogen tetraoxide … Wikipedia
NK-33 — Role: 1st stage multi engine Propellants: RP 1/LOX Development year: 1970 s Overall dimensions Height 3.7 m (12 ft) Diameter … Wikipedia
Walter HWK 109-509 — The HWK 109 509 was a German liquid fuel bipropellant rocket engine that powered Messerschmitt Me 163 and Bachem Ba 349 aircraft. It was produced by Hellmuth Walter Kommanditgesellschaft.It used a two component hypergolic fuel/oxidizer… … Wikipedia