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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