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Template: Engine thrust to weight table. ... Print/export Download as PDF ... Merlin 1D rocket engine, full-thrust version 467 1,030 825 185,000
The designation for a specific motor looks like C6-3.In this example, the letter (C) represents the total impulse range of the motor, the number (6) before the dash represents the average thrust in newtons, and the number (3) after the dash represents the delay in seconds from propelling charge burnout to the firing of the ejection charge (a gas generator composition, usually black powder ...
The following other wikis use this file: Usage on af.wikipedia.org Straalmotor; Usage on ast.wikipedia.org Motor cohete; Usage on ca.wikipedia.org
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A thrust curve for a model rocket. A thrust curve, sometimes known as a "performance curve" or "thrust profile" is a graph of the thrust of an engine or motor, (usually a rocket) with respect to time. [1] [2] Most engines do not produce linear thrust (thrust which increases at a constant rate with time).
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The LR87 was an American liquid-propellant rocket engine used on the first stages of Titan intercontinental ballistic missiles and launch vehicles. [1] Composed of twin motors with separate combustion chambers and turbopump machinery, [2] it is considered a single unit and was never flown as a single combustion chamber engine or designed for this.
Rocket engines in vacuum; Model Type First run Application TSFC I sp (by weight) I sp (by mass) lb/lbf·h g/kN·s s m/s Avio P80: solid fuel: 2006: Vega stage 1 13 360 280 2700 Avio Zefiro 23: solid fuel: 2006: Vega stage 2 12.52 354.7 287.5 2819 Avio Zefiro 9A: solid fuel: 2008: Vega stage 3 12.20 345.4 295.2 2895 Merlin 1D: liquid fuel: 2013 ...