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| | Spacecraft Propulsion Encyclopedia Article, Definition, History, Biography (Site not responding. Last check: 2007-10-26) |
 | | The speed ratio of a rocket nozzle is mostly determined by its area expansion ratio—the ratio of the area of the throat to the area at the exit. |
 | | To improve on this, various exotic nozzle designs such as the plug nozzle, stepped nozzles, the expanding nozzle and the aerospike have been proposed, each having some way to adapt to changing ambient air pressure and each allowing the gas to expand further against the nozzle giving extra thrust at higher altitude. |
 | | Regenerative cooling, where the propellant is passed through tubes around the combustion chamber or nozzle, and other techniques such as curtain cooling or film cooling, may also be employed to give essentially unlimited nozzle life. |
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