EN 16603-32:2014

Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Requirements
Annex A (normative) - Computer aided design
        model description and delivery
        (CADMDD) - DRD
Annex B (normative) - Design loads (DL) - DRD
Annex C (normative) - Dimensional stability analysis
        (DSA) - DRD
Annex D (normative) - Fatigue analysis (FA) - DRD
Annex E (normative) - Fracture control analysis (FCA) - DRD
Annex F (normative) - Fracture control plan - DRD
Annex G (normative) - Fracture control items lists (PFCIL, FCIL
        and FLLIL) - DRD
Annex H (normative) - Material and mechanical part allowables
        (MMPA) - DRD
Annex I (normative) - Mathematical model description and
        delivery (MMDD) - DRD
Annex J (normative) - Modal and dynamic response analysis
        (MDRA) - DRD
Annex K (normative) - Stress and strength analysis (SSA) - DRD
Annex L (normative) - Structure alignment budget (SAB) - DRD
Annex M (normative) - Structure buckling (SB) - DRD
Annex N (normative) - Structure mass summary (SMS) - DRD
Annex O (normative) - Test-analysis correlation (TAC) - DRD
Annex P (normative) - Test evaluation (TE) - DRD
Annex Q (normative) - Test prediction (TP) - DRD
Annex R (informative) - Document description list
Annex S (informative) - Effective mass definition
Annex T (informative) - E-32 discipline documents delivery per
        review
Bibliography

ECSS-E-ST-32C (Space engineering – Structural) defines the mechanical engineering requirements for structural engineering.This Standard specifies the requirements to be considered in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, in­service and eventual disposal.The Standard applies to all general structural subsystem aspects of space products including: launch vehicles, transfer vehicles, re­entry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems.This Standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS S ST-00.