固体弹道导弹与运载火箭概念设计

本书特色

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Solid Ballistic Missile and Launch Vehicle Conceptual Design固体弹道导弹与运载火箭概念设计Themaincontentsofthisbookincludetheessentialprinciplesinvolvedintheconceptualdesignofsolidballisticmissileandlaunchvehicle.Thebookisdividedintothreeparts.Thefirstpartgivesbasicandusefulmethodofsolidballisticmissileconceptualdesign.Thesolidlaunchvehicleconceptualdesignmethodwhichissuitabletoarrangesmallsizesatellitelaunchingisdescribedinsecondpart.Thethirdpartpresentsfundamentalsofrocketballisticswhichcanbeusedtocalculatethetrajectoriesofballisticmissileandlaunchvehicle.Thisbookistendedforseniorundergraduateandpostgraduatestudentswhoneedtohavecertainprogrammingability.Thebookisalsousefultoyoungengineerswhohopetostudysomebasicknowledgeinthisfield.

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目录

PartOne SolidBallisticMissileDesign
Chapter1 Introduction …………………………………………………………………… 3
1.1 System（s）Engineering（SE） ……………………………………………………… 3
1.2 ConcurrentEngineering（CE） ……………………………………………………… 4
1.3 Conceptof（Solid）BallisticMissile………………………………………………… 6
1.4 DesignRequirementsofBallisticMissile ………………………………………… 10
ProblemsofChapter1 …………………………………………………………………… 16
Chapter2 MassModelofSolidBallisticMissile …………………………………… 17
2.1 MassEquationofSolidBallisticMissile ………………………………………… 17
2.2 CalculationoftheStructuralCoefficientofaSRM ……………………………… 21
ProblemsofChapter2 …………………………………………………………………… 33
Chapter3 TrajectoryModelofSolidBallisticMissile……………………………… 34
3.1 CoordinateSystems（Frames）……………………………………………………… 34
3.2 EquationsofMotioninPoweredFlightPhaseofBM Trajectory ……………… 35
3.3 EquationsofMotioninFreeFlightPhaseofaBM …………………………… 42
ProblemsofChapter3 …………………………………………………………………… 43
Chapter4 OptimizationofTrajectory ………………………………………………… 44
4.1 RequirementsforFlightProgram ………………………………………………… 44
4.2 DesignofFlightProgram ………………………………………………………… 46
4.3 TrajectoryOptimization …………………………………………………………… 52
ProblemsofChapter4 …………………………………………………………………… 59
Chapter5 OptimizationofOverallParameters ……………………………………… 60
5.1 SelectionofOverallOptimizationDesignParameters…………………………… 60
5.2 SelectionofDesignParameters …………………………………………………… 68
5.3 MathematicModeloftheSchemeDesignOptimization ………………………… 72
5.4 EPFM Method ……………………………………………………………………… 75
ProblemsofChapter5 …………………………………………………………………… 81
Chapter6 ExampleofOverallParametersOptimization ………………………… 82
6.1 BasicParameters …………………………………………………………………… 82
6.2 ResultsoftheOptimization ……………………………………………………… 84
ProblemsofChapter6 …………………………………………………………………… 86
Chapter7 Re-entryVehicleDesign …………………………………………………… 87
7.1 Introduction ………………………………………………………………………… 87
7.2 GeneralEquationofMotion ……………………………………………………… 90
7.3 ApproximateRe-entryTrajectory ……………………………………………… 100
7.4 Maximum AxialOverloadCoefficient…………………………………………… 105
7.5 EffectiveFactorsonRe-entryTrajectory ……………………………………… 108
7.6 Re-entryHeatingProblem ……………………………………………………… 114
ProblemsofChapter7…………………………………………………………………… 122
Chapter8 Re-entryBodyManeuver…………………………………………………… 123
8.1 ConceptofAnti-BallisticMissileSystem （ABMS） …………………………… 123
8.2 ConceptofCountermeasurestoNMD …………………………………………… 123
8.3 ConceptofManeuverFlightofReentryBody ………………………………… 125
ProblemsofChapter8…………………………………………………………………… 126
PartTwo SolidLaunchVehicleDesign
Chapter9 IntroductionofSolidLaunchVehicle …………………………………… 129
9.1 ConceptofSolidLaunchVehicle（SLV）………………………………………… 129
9.2 SomeExamples …………………………………………………………………… 131
9.3 OutlineofSolidLaunchVehicleDesignProcess ……………………………… 133
ProblemsofChapter9…………………………………………………………………… 134
Chapter10 OrbitInsertionofSLV …………………………………………………… 135
10.1 InsertionMethod ………………………………………………………………… 135
10.2 FlightProgram …………………………………………………………………… 136
10.3 TheFlightParametersoftheSLVattheApex ……………………………… 137
10.4 AccelerationFlightPhaseofSLVInsertion…………………………………… 140
ProblemsofChapter10 ………………………………………………………………… 142
Chapter11 MassModelofSLV ……………………………………………………… 143
11.1 MassEquationofaSLV ………………………………………………………… 143
11.2 TheMassofGrain（SolidPropellants）………………………………………… 143
11.4 TheMassEquationoftheithStageRocket（Subrocket）…………………… 151
11.5 TheExpressionofFillingCoefficient ………………………………………… 152
11.6 TheMassEquationoftheithStageRocketofaSLV ……………………… 162
ProblemsofChapter11 ………………………………………………………………… 162
Chapter12 ConceptualDesignofSLV ……………………………………………… 163
12.1 DesignMission …………………………………………………………………… 163
12.2 InjectionDesign ………………………………………………………………… 164
12.3 TheRequiredOrbitVelocity …………………………………………………… 165
12.4 TheBoundsoftheZoneofTolerableVelocity ……………………………… 165
12.5 AccordingtothePayloadMasstoDeterminetheCoefficient ……………… 168
12.6 OptimizationofMassDistribution……………………………………………… 169
ProblemsofChapter12 ………………………………………………………………… 177
PartThree FoundationsofRocketBallistics
Chapter13 EnvironmentofFlightforRocketandSpacecraft ………………… 181
13.1 TheEarthAtmosphere ………………………………………………………… 181
13.2 TheEarthGravitationalField ………………………………………………… 184
13.3 TheReferenceEllipsoidModelofEarth ……………………………………… 185
ProblemsofChapter13 ………………………………………………………………… 187
Chapter14 EquationofMotionofRocket ………………………………………… 188
14.1 CoordinateSystem （Frames）UsedinRocketBallistics……………………… 188
14.2 VectorFormofEquationofMotionofRocketCenterofMass …………… 191
14.3 ScalarFormofEquationofMotionofRocketCenterofMass ……………… 191
14.4 EquationofRotationalMotionofRocket……………………………………… 194
14.5 AdditionalEquations …………………………………………………………… 196
ProblemsofChapter14 ………………………………………………………………… 197
Chapter15 PassiveFlightPhaseofRocket ………………………………………… 198
15.1 TransformationofPositionandVelocityofBurn-outPoint ………………… 198
15.2 Free-flightTrajectory …………………………………………………………… 199
15.3 SimplifiedAnalysis ……………………………………………………………… 202
15.4 TimeofFreeFlight……………………………………………………………… 203
15.5 RecentlyTrajectory ……………………………………………………………… 203
15.6 PositionofImportPoint ………………………………………………………… 204
15.7 InfluenceCoefficientsofImpactPointDeviation……………………………… 204
ProblemsofChapter15 ………………………………………………………………… 206
AppendixA SimpleMethodforMassEstimationofSRM CaseforConceptual
Design ……………………………………………………………………… 207
A.1 SphericalClosure ………………………………………………………………… 207
A.2 EllipsoidClosure ………………………………………………………………… 208
A.3 CylindricalSection ……………………………………………………………… 208
A.4 GlassFilamentWoundCase（Semi-empiricalFormulas）……………………… 209
AppendixB VelocityandAccelerationinaMovingFrame ……………………… 210
References …………………………………………………………………………………… 211

封面

书名:固体弹道导弹与运载火箭概念设计

作者:何麟书

页数:未知

定价:¥55.0

出版社:北京航空航天大学出版社

出版日期:暂无

ISBN:9787512423183

PDF电子书大小:57MB 高清扫描完整版