固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] epub pdf mobi txt 電子書 下載 2024

固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] epub pdf mobi txt 電子書 下載 2024

☆☆☆☆☆
簡體網頁||繁體網頁



點擊這裡下載

固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] epub pdf mobi txt 電子書 下載 2024

类似图書 點擊查看全場最低價

---

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

固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design] epub pdf mobi txt 電子書 下載 2024

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

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

評分☆☆☆☆☆

還行

类似图書 點擊查看全場最低價