固体弹道导弹与运载火箭概念设计 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] 下载 mobi epub pdf 电子书 2024

☆☆☆☆☆
简体网页||繁体网页



点击这里下载

类似图书 点击查看全场最低价

---

内容简介

　　Solid Ballistic Missile and Launch Vehicle Conceptual Design　　固体弹道导弹与运载火箭概念设计　　Themaincontentsofthisbookincludetheessentialprinciplesinvolvedintheconceptualdesignofsolid　　ballisticmissileandlaunchvehicle.　　Thebookisdividedintothreeparts.Thefirstpartgivesbasicandusefulmethodofsolidballisticmissile　　conceptualdesign.Thesolidlaunchvehicleconceptualdesignmethodwhichissuitabletoarrangesmallsize　　satellitelaunchingisdescribedinsecondpart.Thethirdpartpresentsfundamentalsofrocketballisticswhich　　canbeusedtocalculatethetrajectoriesofballisticmissileandlaunchvehicle.　　Thisbookistendedforseniorundergraduateandpostgraduatestudentswhoneedtohavecertainprogramming　　ability.Thebookisalsousefultoyoungengineerswhohopetostudysomebasicknowledgeinthisfield.

目录

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
固体弹道导弹与运载火箭概念设计 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] 下载 mobi epub pdf txt 电子书 格式

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

评分☆☆☆☆☆

还行

类似图书 点击查看全场最低价