NASA STD 5012:2006

NASA STD 5012:2006 Strength And Life Assessment Requirements For Liquid Fueled Space Propulsion System Engines Provides strength and life assessment requirements for National Aeronautics and Space Administration (NASA) liquid fueled space propulsion system engines.

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Table of Contents

DOCUMENTHISTORYLOG
FOREWORD
1.SCOPE
1.1Purpose
1.2Applicability
2.APPLICABLEDOCUMENTS
2.1General
2.2GovernmentDocuments
2.3Non-GovernmentDocuments
2.4OrderofPrecedence
3.ACRONYMSANDDEFINITIONS
3.1Acronyms
3.2Definitions
4.REQUIREMENTS
4.1GeneralRequirements
4.1.1StrengthandLifeAssessments
4.1.2GroundSupportEquipment(GSE)andFlight
SupportEquipment(FSE)
4.1.3TransportationofFlightStructures
4.2DetailedRequirements
4.2.1StrengthAnalysis
4.2.1.1LoadConditions
4.2.1.2Materials
4.2.1.3DesignandAnalysisThickness
4.2.1.4WeldandBrazeJoints
4.2.1.5BucklingandCrippling
4.2.1.6FastenersandPreloadedJoints
4.2.1.7HardwarethatExperiencesPressure
Loading
4.2.1.8CompositeandBondedStructures
4.2.1.9FactorsofSafety
4.2.1.10MarginsofSafety
4.2.1.11OtherDesignFactors
4.2.1.12LocalYielding
4.2.2StrengthTests
4.2.2.1DevelopmentTests
4.2.2.2QualificationTests
4.2.2.3Acceptance/ProofTests
4.2.2.4Test-LevelCorrectionsforEnvironment
4.2.3FactorsofSafetyforAnalysisandStrength
TestFactors
4.2.4LifeAnalysis
4.2.4.1MaterialProperties
4.2.4.2LoadsSpectra
4.2.4.3CreepAnalysis
4.2.4.4FatigueAnalysis
4.2.4.5FatigueTests
4.2.5Documentation
4.2.5.1StructuralAssessmentPlan
4.2.5.2AnalysesandTestReports

Abstract

Provides strength and life assessment requirements for National Aeronautics and Space Administration (NASA) liquid fueled space propulsion system engines.

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