固體彈道導彈與運載火箭概念設計 [Solid Ballistic Missile and Launch Vehicle Conceptual Design]

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 mobi epub pdf 電子書 2024


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圖書介紹

齣版社: 北京航空航天大學齣版社
ISBN:9787512423183
版次:1
商品編碼:12030313
包裝:平裝
外文名稱:Solid Ballistic Missile and Launch Vehicle Conceptual Design
開本:16開
齣版時間:2017-01-01
用紙:膠版紙


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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] 下載 mobi epub pdf txt 電子書 格式

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