Printer Friendly
Dictionary, Encyclopedia and Thesaurus - The Free Dictionary
3,922,768,675 visitors served.
forum Join the Word of the Day Mailing List For webmasters
?
Dictionary/
thesaurus
Medical
dictionary
Legal
dictionary
Financial
dictionary
Acronyms
 
Idioms
Encyclopedia
Wikipedia
encyclopedia
?

Nuclear Rocket Engine

    0.03 sec.
Nuclear Rocket Engine 

a rocket engine in which thrust is produced by the energy released in radioactive decay or a nuclear reaction. Depending on the type of nuclear reaction used in the engine, a distinction is made between radioisotope rocket engines, thermonuclear rocket engines, and nuclear rocket engines proper (nuclear-fission rocket engines).

A nuclear-fission rocket engine consists of a reactor, nozzle, turbopump unit for feeding the working fluid to the reactor from the tank of the propulsion unit (where it is stored as a liquid), control units, and other elements. In the nuclear reactor the working fluid is converted to a high-temperature gas that creates thrust as it escapes. The gas for driving the turbopump unit can be produced by heating the main working fluid in the reactor. The nozzle of the turbopump unit and many other units of a nuclear-fission rocket engine are similar to the corresponding units of liquid-propellant rocket engines. The fundamental difference lies in the use of a nuclear reactor instead of a combustion chamber. The advantage of the nuclear-fission rocket engine is the high specific impulse derived from the high exhaust velocity of the working fluid, which reaches 50 km/sec or more. The resulting specific impulse is much higher than in chemical rocket engines, in which the exhaust velocity of the working fluid does not exceed 4.5 km/sec. The US experimental rocket engine Nerva-1, in the developmental stage in 1977, weighs 11 tons and develops a thrust of more than 300 kilonewtons with a specific impulse of 8.1 km/sec. Experimental models of radioisotope rocket engines with thrust ratings with a specific impulse up to several newtons had been developed by 1978. All types of nuclear rocket engines are intended for operation only in outer space.

REFERENCES

Bussard, R. W. and R. D. De Lauer. Raketa s atomnym dvigatelem. Moscow, 1960. (Translated from English.)
Bussard, R. W., and R. D. De Lauer. Iadernye dvigateli dlia samoletov i raket. Moscow, 1967. (Translated from English.)


Want to thank TFD for its existence? Tell a friend about us, add a link to this page, add the site to iGoogle, or visit the webmaster's page for free fun content.
?Page tools
Printer friendly
Cite / link
Feedback
Mentioned in?  References in periodicals archive?   Encyclopedia browser?   Full browser?
No references found
 
68 TL783 Dewar describes how the US nuclear rocket engine program, Project Rover/NERVA, operated from 1955 to 1973, then was mercilessly stabbed in the back by villainous politicians whose ultimate goal was to destroy the entire US space program.
The leading current-technology candidate for a new propulsion source is the nuclear rocket engine, which was researched but never flight-tested for the Apollo program.
The leading current-technology candidate for a new propulsion source is the nuclear rocket engine, which was researched but never flight-tested for the Apollo program.
 
 
 
Encyclopedia
?

Terms of Use | Privacy policy | Feedback | Advertise with Us | Copyright © 2012 Farlex, Inc.
Disclaimer
All content on this website, including dictionary, thesaurus, literature, geography, and other reference data is for informational purposes only. This information should not be considered complete, up to date, and is not intended to be used in place of a visit, consultation, or advice of a legal, medical, or any other professional.