generalized theory of rocket propulsion for future space travel外语英文电子书

generalized theory of rocket propulsion for future space travel外语英文电子书

ID:8054596

大小:1.36 MB

页数:9页

时间:2018-03-05

generalized theory of rocket propulsion for future space travel外语英文电子书_第1页
generalized theory of rocket propulsion for future space travel外语英文电子书_第2页
generalized theory of rocket propulsion for future space travel外语英文电子书_第3页
generalized theory of rocket propulsion for future space travel外语英文电子书_第4页
generalized theory of rocket propulsion for future space travel外语英文电子书_第5页
资源描述:

《generalized theory of rocket propulsion for future space travel外语英文电子书》由会员上传分享,免费在线阅读,更多相关内容在教育资源-天天文库

1、320J.PROPULSIONVOL.3,NO.4GeneralizedTheoryofRocketPropulsionforFutureSpaceTravelMichaelA.Minovitch*PhaserTelepropulsion,Inc.,LosAngeles,CaliforniaThispaperintroducesageneralizedtheoryofclassicalrocketpropulsionforreusablespacevehicleswhereinthepropellantisatmosphericgas

2、andthepropulsivedeceleratingoracceleratingthrustisgeneratedby,respec-tively,ingestingorexpellingatmosphericgasathighvelocities.Theworkingfluidexpelledduringacceleratingpropulsivemaneuversisautomaticallyreplenishedduringdeceleratingpropulsivemaneuvers.Therefuelingretroth

3、rustisgeneratedbyalarge-diameterhypervelocitygasinletdiffusermountedatthefrontofthevehicle,whichingestsgaswhiletraversingthroughthetenuousupperregionsofaplanet'satmosphere.Thevehicletherebytransfersaportionofitsmomentumtothecollectedgas,whichwasinitiallyatrestintheatmos

4、phere.Thistransferofmomentumgeneratesadeceleratingretrothrustbyareverseapplicationofthetheoryofclassicalrocketpropulsion.Theingestedgasisliquefied,storedonboardthevehicle,andutilizedasapropellantforgeneratingtheacceleratingthrustbyelectricallyacceleratingandexpellingthe

5、gasathighvelocities.Byexpellingthegaswithavelocityexceedingtheinletvelocity,thevehiclebecomesself-refueling.Thevehiclecouldoperateeitherasaself-refuelinginterorbitaltransfervehicleorasaninterplanetarytransfervehiclemovingfromplanettoplanetutilizingeachplanetaryatmospher

6、easpropulsiveworkingfluid.Introductionandthe"massratio"isgivenbythewell-known"rocketTHEfundamentalphysicalprinciplethatallspacepropul-equation,"sionsystemsutilizeforgeneratingpropulsivethrustisbasedonNewton'sthirdlawofmotion:"Foreveryaction(3)thereisanequalandoppositere

7、action."Accordingtothepresentlyconceivedtheoryofrocketpropulsion(whichwillbewhereMlandM2denotethevehicle'smassbeforeandafterreferredtoasthe"classicaltheoryofrocketpropulsion"),expellinganamountofpropellantmp=Mt—M2toachieveaNewton'sprincipleisalwaysappliedinonedirection—

8、expel-velocitychangeAV.lingmass(i.e.,propellant)storedonboardthevehicle,outofItfollowsdirectlyfromEq.(3)thatth

当前文档最多预览五页,下载文档查看全文

此文档下载收益归作者所有

当前文档最多预览五页,下载文档查看全文
温馨提示:
1. 部分包含数学公式或PPT动画的文件,查看预览时可能会显示错乱或异常,文件下载后无此问题,请放心下载。
2. 本文档由用户上传,版权归属用户,天天文库负责整理代发布。如果您对本文档版权有争议请及时联系客服。
3. 下载前请仔细阅读文档内容,确认文档内容符合您的需求后进行下载,若出现内容与标题不符可向本站投诉处理。
4. 下载文档时可能由于网络波动等原因无法下载或下载错误,付费完成后未能成功下载的用户请联系客服处理。