固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] pdf epub mobi txt 电子书 下载 2025

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何麟書，徐大軍 著

齣版社： 北京航空航天大學齣版社

ISBN：9787512423183

版次：1

商品編碼：12030313

包裝：平裝

外文名稱：Solid Ballistic Missile and Launch Vehicle Conceptual Design

開本：16開

齣版時間：2017-01-01

用紙：膠版紙

內容簡介

　　Solid Ballistic Missile and Launch Vehicle Conceptual Design　　固體彈道導彈與運載火箭概念設計　　Themaincontentsofthisbookincludetheessentialprinciplesinvolvedintheconceptualdesignofsolid　　ballisticmissileandlaunchvehicle.　　Thebookisdividedintothreeparts.Thefirstpartgivesbasicandusefulmethodofsolidballisticmissile　　conceptualdesign.Thesolidlaunchvehicleconceptualdesignmethodwhichissuitabletoarrangesmallsize　　satellitelaunchingisdescribedinsecondpart.Thethirdpartpresentsfundamentalsofrocketballisticswhich　　canbeusedtocalculatethetrajectoriesofballisticmissileandlaunchvehicle.　　Thisbookistendedforseniorundergraduateandpostgraduatestudentswhoneedtohavecertainprogramming　　ability.Thebookisalsousefultoyoungengineerswhohopetostudysomebasicknowledgeinthisfield.

目錄

PartOne SolidBallisticMissileDesignChapter1 Introduction …………………………………………………………………… 31.1 System（s）Engineering（SE） ……………………………………………………… 31.2 ConcurrentEngineering（CE） ……………………………………………………… 41.3 Conceptof（Solid）BallisticMissile………………………………………………… 61.4 DesignRequirementsofBallisticMissile ………………………………………… 10ProblemsofChapter1 …………………………………………………………………… 16Chapter2 MassModelofSolidBallisticMissile …………………………………… 172.1 MassEquationofSolidBallisticMissile ………………………………………… 172.2 CalculationoftheStructuralCoefficientofaSRM ……………………………… 21ProblemsofChapter2 …………………………………………………………………… 33Chapter3 TrajectoryModelofSolidBallisticMissile……………………………… 343.1 CoordinateSystems（Frames）……………………………………………………… 343.2 EquationsofMotioninPoweredFlightPhaseofBM Trajectory ……………… 353.3 EquationsofMotioninFreeFlightPhaseofaBM …………………………… 42ProblemsofChapter3 …………………………………………………………………… 43Chapter4 OptimizationofTrajectory ………………………………………………… 444.1 RequirementsforFlightProgram ………………………………………………… 444.2 DesignofFlightProgram ………………………………………………………… 464.3 TrajectoryOptimization …………………………………………………………… 52ProblemsofChapter4 …………………………………………………………………… 59Chapter5 OptimizationofOverallParameters ……………………………………… 605.1 SelectionofOverallOptimizationDesignParameters…………………………… 605.2 SelectionofDesignParameters …………………………………………………… 685.3 MathematicModeloftheSchemeDesignOptimization ………………………… 725.4 EPFM Method ……………………………………………………………………… 75ProblemsofChapter5 …………………………………………………………………… 81Chapter6 ExampleofOverallParametersOptimization ………………………… 826.1 BasicParameters …………………………………………………………………… 826.2 ResultsoftheOptimization ……………………………………………………… 84ProblemsofChapter6 …………………………………………………………………… 86Chapter7 Re-entryVehicleDesign …………………………………………………… 877.1 Introduction ………………………………………………………………………… 877.2 GeneralEquationofMotion ……………………………………………………… 907.3 ApproximateRe-entryTrajectory ……………………………………………… 1007.4 Maximum AxialOverloadCoefficient…………………………………………… 1057.5 EffectiveFactorsonRe-entryTrajectory ……………………………………… 1087.6 Re-entryHeatingProblem ……………………………………………………… 114ProblemsofChapter7…………………………………………………………………… 122Chapter8 Re-entryBodyManeuver…………………………………………………… 1238.1 ConceptofAnti-BallisticMissileSystem （ABMS） …………………………… 1238.2 ConceptofCountermeasurestoNMD …………………………………………… 1238.3 ConceptofManeuverFlightofReentryBody ………………………………… 125ProblemsofChapter8…………………………………………………………………… 126PartTwo SolidLaunchVehicleDesignChapter9 IntroductionofSolidLaunchVehicle …………………………………… 1299.1 ConceptofSolidLaunchVehicle（SLV）………………………………………… 1299.2 SomeExamples …………………………………………………………………… 1319.3 OutlineofSolidLaunchVehicleDesignProcess ……………………………… 133ProblemsofChapter9…………………………………………………………………… 134Chapter10 OrbitInsertionofSLV …………………………………………………… 13510.1 InsertionMethod ………………………………………………………………… 13510.2 FlightProgram …………………………………………………………………… 13610.3 TheFlightParametersoftheSLVattheApex ……………………………… 13710.4 AccelerationFlightPhaseofSLVInsertion…………………………………… 140ProblemsofChapter10 ………………………………………………………………… 142Chapter11 MassModelofSLV ……………………………………………………… 14311.1 MassEquationofaSLV ………………………………………………………… 14311.2 TheMassofGrain（SolidPropellants）………………………………………… 14311.4 TheMassEquationoftheithStageRocket（Subrocket）…………………… 15111.5 TheExpressionofFillingCoefficient ………………………………………… 15211.6 TheMassEquationoftheithStageRocketofaSLV ……………………… 162ProblemsofChapter11 ………………………………………………………………… 162Chapter12 ConceptualDesignofSLV ……………………………………………… 16312.1 DesignMission …………………………………………………………………… 16312.2 InjectionDesign ………………………………………………………………… 16412.3 TheRequiredOrbitVelocity …………………………………………………… 16512.4 TheBoundsoftheZoneofTolerableVelocity ……………………………… 16512.5 AccordingtothePayloadMasstoDeterminetheCoefficient ……………… 16812.6 OptimizationofMassDistribution……………………………………………… 169ProblemsofChapter12 ………………………………………………………………… 177PartThree FoundationsofRocketBallisticsChapter13 EnvironmentofFlightforRocketandSpacecraft ………………… 18113.1 TheEarthAtmosphere ………………………………………………………… 18113.2 TheEarthGravitationalField ………………………………………………… 18413.3 TheReferenceEllipsoidModelofEarth ……………………………………… 185ProblemsofChapter13 ………………………………………………………………… 187Chapter14 EquationofMotionofRocket ………………………………………… 18814.1 CoordinateSystem （Frames）UsedinRocketBallistics……………………… 18814.2 VectorFormofEquationofMotionofRocketCenterofMass …………… 19114.3 ScalarFormofEquationofMotionofRocketCenterofMass ……………… 19114.4 EquationofRotationalMotionofRocket……………………………………… 19414.5 AdditionalEquations …………………………………………………………… 196ProblemsofChapter14 ………………………………………………………………… 197Chapter15 PassiveFlightPhaseofRocket ………………………………………… 19815.1 TransformationofPositionandVelocityofBurn-outPoint ………………… 19815.2 Free-flightTrajectory …………………………………………………………… 19915.3 SimplifiedAnalysis ……………………………………………………………… 20215.4 TimeofFreeFlight……………………………………………………………… 20315.5 RecentlyTrajectory ……………………………………………………………… 20315.6 PositionofImportPoint ………………………………………………………… 20415.7 InfluenceCoefficientsofImpactPointDeviation……………………………… 204ProblemsofChapter15 ………………………………………………………………… 206AppendixA SimpleMethodforMassEstimationofSRM CaseforConceptualDesign ……………………………………………………………………… 207A.1 SphericalClosure ………………………………………………………………… 207A.2 EllipsoidClosure ………………………………………………………………… 208A.3 CylindricalSection ……………………………………………………………… 208A.4 GlassFilamentWoundCase（Semi-empiricalFormulas）……………………… 209AppendixB VelocityandAccelerationinaMovingFrame ……………………… 210References …………………………………………………………………………………… 211

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