engine thrust-to-weight ratio

engine thrust-to-weight ratio
удельная тяга двигателя

Англо-русский словарь промышленной и научной лексики. 2014.

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  • Thrust-to-weight ratio — is, as its name suggests, the ratio of instantaneous thrust to weight (where weight means weight at the Earth’s surfaceSutton (7th edition pg 442) thrust to weight ratio F/Wg is a dimensionless parameter that is identical to the acceleration of… …   Wikipedia

  • thrust-weight/thrust/weight ratio — The ratio of the maximum sea level static installed thrust to aircraft weight. It is one of the combat performance attributes that gives an idea of the maneuverability of a combat aircraft. This ratio is generally greater than one in air… …   Aviation dictionary

  • Thrust — is a reaction force described quantitatively by Newton s Second and Third Laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.ExamplesA fixed wing… …   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

  • Jet engine — For a general overview of aircraft engines, see Aircraft engine. A Pratt Whitney F100 turbofan engine for the …   Wikipedia

  • Aircraft engine — An aircraft engine is a propulsion system for an aircraft. Aircraft engines are almost always a type of lightweight internal combustion engine. This article is an overview of the basic types of aircraft engines and the design concepts employed in …   Wikipedia

  • Internal combustion engine — The internal combustion engine is an engine in which the combustion of a fuel (normally a fossil fuel) occurs with an oxidizer (usually air) in a combustion chamber. In an internal combustion engine, the expansion of the high temperature and high …   Wikipedia

  • Merlin (rocket engine) — Merlin 1C SpaceX Merlin 1A (shown) Country of origin United States Manufacturer SpaceX Liq …   Wikipedia

  • RD-170 (rocket engine) — The RD 170 is the world s most powerful multi nozzle multi chamber liquid bipropellant rocket engine. It burns the Russian equivalent of RP 1 fuel and LOX oxidizer in four combustion chambers supplied by a single turbo pump according to a staged… …   Wikipedia

  • RS-27A (rocket engine) — The RS 27A is a medium sized rocket engine developed by Rocketdyne for use on the Delta II and Delta III rockets. It is fueled by a kerosene / LOX mixture in a gas generator cycle. The engine is a modified version of its predecessor, the RS 27;… …   Wikipedia

  • Engine Alliance GP7000 — The Engine Alliance GP7000 (known as the GP7200 for a brief time period) is a new turbofan jet engine that will incorporate advanced technologies of proven wide body products, originally from the world s No.1 and No.3 aero engine manufacturers,… …   Wikipedia


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