A rocket engine is a reaction engine that produces thrust, in accordance with Newton's third law, by ejecting reaction mass rearward, typically through a combustion chamber, injectors and a nozzle that accelerates hot gases to generate forward motion. Unlike a jet engine, a rocket engine carries its own oxidizer, letting it operate outside the atmosphere, which is the property that makes spaceflight possible. Modern liquid-propellant rocket engine development accelerated through the 20th century in the United States and the Soviet Union; the first American liquid-propellant rocket engine company, Reaction Motors Inc., was founded in 1941, and rocket engines went on to power the Saturn V program from 1961 to 1975 and the Space Shuttle from 1981 to 2011.
Facts
YearSourced to the subject's own account SignificanceSourced to the subject's own accountGoddard's use of a De Laval nozzle on a solid-propellant rocket engine, which doubled its thrust and cut fuel needs by a factor of about 25, marked the birth of the modern rocket engine. 1 Connections
Associated With
Inconel, Materials Inconel is used in rocket engine combustion chambers and nozzles for high-temperature, high-stress service.
In Field
Source Rocket Engine (Wikipedia)
Invented By
Sources
1. Rocket Engine (Wikipedia)
WikipediaHistory section, Goddard paragraph 2, sentence 1
Goddard began to use liquid propellants in 1921, and in 1926 became the first to launch a liquid-fuelled rocket.
History section, Goddard paragraph 1, sentence 3
This was the birth of the modern rocket engine.
- In Group: Rocket and Launch Vehicle Propulsion Systems, lead: reaction engine producing thrust by ejecting a high-speed jet of hot combustion gas
In Field: Aerospace Engineering, Categories
Aerospace technologies
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