《固體彈道飛彈與運載火箭概念設計》是2017年1月北京航空航天大學出版社出版的圖書，作者是何麟書、徐大軍。
基本介紹
- 中文名：固體彈道飛彈與運載火箭概念設計
- 作者：何麟書、徐大軍
- 出版社：北京航空航天大學出版社
- 出版時間：2017年1月
- 定價：55 元
- 開本：16 開
- 裝幀：平裝
- ISBN：9787512423183
內容簡介,圖書目錄,
內容簡介
Themaincontentsofthisbookincludetheessentialprinciplesinvolvedintheconceptualdesignofsolid
ballisticmissileandlaunchvehicle.
Thebookisdividedintothreeparts.Thefirstpartgivesbasicandusefulmethodofsolidballisticmissile
conceptualdesign.Thesolidlaunchvehicleconceptualdesignmethodwhichissuitabletoarrangesmallsize
satellitelaunchingisdescribedinsecondpart.Thethirdpartpresentsfundamentalsofrocketballisticswhich
canbeusedtocalculatethetrajectoriesofballisticmissileandlaunchvehicle.
Thisbookistendedforseniorundergraduateandpostgraduatestudentswhoneedtohavecertainprogramming
ability.Thebookisalsousefultoyoungengineerswhohopetostudysomebasicknowledgeinthisfield.
圖書目錄
PartOne SolidBallisticMissileDesign
Chapter1 Introduction ……炒刪鞏棵……………………………………………………………… 3
1.1 System（s）Engineering（SE） ……………………………………………乃鑽套奔………… 3
1.2 ConcurrentEngineering（CE） …………………………多芝紋…………………………笑體催… 4
1.3 Conceptof（Solid）BallisticMissile………………………………………………… 6
1.4 DesignRequirementsofBallisticMissile ………………………………………… 10
ProblemsofChapter1 ………………………芝舉…………………牛坑鞏………………………… 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 ……………………………………………………婚求剃……… 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
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
