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With this software you can investigate how a rocket nozzle produces thrust by changing the values of different factors that affect thrust.
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exploration.grc.nasa.gov/education/rocket/ienzl.html
exploration.grc.nasa.gov/education/rocket/ienzl.html
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The amount of thrust produced by the rocket depends on the mass flow rate through the engine, the exit velocity of the exhaust, and the pressure at the nozzle exit. All of these variables depend on the design of the nozzle.
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www.grc.nasa.gov/WWW/K-12/airplane/rockth.html
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The thrust of the rocket is given by the theoretical equation : ... The specific impulse Isp of a rocket is the parameter that determines the overall effectiveness of the rocket nozzle and propellant. It is defined as the ratio of the thrust and the propellant weight flow rate, or...
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www.aticourses.com/rocket_tutorial.htm
www.aticourses.com/rocket_tutorial.htm
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The space shuttle is often said to be the most advanced traveling machine ever built, but most of its rocket thrust comes from a design essentially unchanged in 800 years.
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www.rense.com/general2/thrust.htm
www.rense.com/general2/thrust.htm
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How much thrust does a rocket need in take off? ... How much thrust did Apollo 11 rocket have? ... What does a rocket thrust ring do?
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www.answers.com/topic/rocket-thrust
www.answers.com/topic/rocket-thrust
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This is the first major publication on liquid-rocket combustion devices since 1960, and includes 20 chapters prepared by world-renowned experts. Each chapter focuses on a specific aspect of liquid-propellant combustion and thrust chamber dynamics, ... Liquid Rocket Thrust Chambers: Aspects of Modeling, Analysis, and Design...
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www.aiaa.org/content.cfm?pageid=360&id=1002
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View Patent Images: ... Images are available in PDF form when logged in. To view PDFs, Login or Create Account (Free!) ... United States Patent 3179123...
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www.freepatentsonline.com/3179123.html
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Rocket - Wikipedia, the free encyclopedia
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A rocket or rocket vehicle is a missile, spacecraft, aircraft or other vehicle which obtains thrust by the reaction of the rocket to the ejection of fast moving fluid exhaust from a rocket engine....
en.wikipedia.org/wiki/Rocket
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Rocket thrust results from the high speed ejection of material and does not require any medium to "push against". Conservation of momentum dictates that if material is ejected backward, the forward momentum of the remaining rocket must increase since an isolated system cannot change its net momentum.
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hyperphysics.phy-astr.gsu.edu/HBASE/rocket.html
hyperphysics.phy-astr.gsu.edu/HBASE/rocket.html
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