Technology and Engineering Atlas

How Things Are Built
Sign In
Text size
100%
Theme
Invention

Rocket Engine

Aerospace Engineering

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
1926 1
SignificanceSourced to the subject's own account
Goddard'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)
Wikipedia
  • History 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
View the Source
Comments (0)
No comments yet. Be the first to share a thought.
Reader Challenges (0)
No disputes yet. Spotted an error or a better source? Open the first one.