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EN 14824:2003

Superseded
Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space engineering - Testing
Superseded date

08-01-2014

Published date

12-10-2003

Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
   3.1 Terms and definitions
   3.2 Abbreviated terms
4 General requirements
   4.1 Testing philosophy
   4.2 Model philosophy
   4.3 Development testing
   4.4 Qualification testing
   4.5 Acceptance testing
   4.6 Protoflight testing
   4.7 Retesting
   4.8 Test conditions and tolerances
   4.9 Operations validation testing
   4.10 Test data
   4.11 Test documentation
5 Qualification testing
   5.1 Equipment test requirements
   5.2 Subsystem test requirements
   5.3 Element test requirements
   5.4 System qualification test
6 Acceptance testing
   6.1 Equipment test requirements
   6.2 Subsystem test requirements
   6.3 Element test requirements
   6.4 System test requirements
7 Protoflight testing
   7.1 Equipment test requirements
   7.2 Subsystem test requirements
   7.3 Element test requirements
   7.4 System test requirements
8 Pre-launch testing
   8.1 General
   8.2 Functional tests
   8.3 Propulsion tests
   8.4 Integrated launch system test
   8.5 Manned related tests
9 In-orbit testing
10 Post-landing testing
Annex A (informative) Mechanical and vibration testing for
                      space equipment
      A.1 Derivation of qualification test levels for units
          from mechanical test data analysis
          A.1.1 Introduction
          A.1.2 Unit level random testing
          A.1.3 Unit level sinusoidal testing
          A.1.4 References
      A.2 Vibration test philosophy
      A.3 Technical information on mechanical test factors
          A.3.1 Introduction
          A.3.2 References
          A.3.3 Loads
          A.3.4 Margin of safety
      A.4 Microgravity environment compatibility (MEC)
          A.4.1 Introduction
          A.4.2 Disturbance source definition
          A.4.3 MEC control approach
Annex B (informative) Temperature limits and test levels for
                      space equipment
      B.1 Introduction
      B.2 References
      B.3 Influence of equipment temperature limits on thermal
          design
      B.4 Verification by analysis concerning accuracy and
          level of confidence
          B.4.1 General philosophy of uncertainty application
          B.4.2 Temperature uncertainty determination
          B.4.3 Quantification of uncertainty values
          B.4.4 Test correlation criteria
      B.5 Standardization of equipment temperature limits
          B.5.1 Evaluation and classification of equipment data
          B.5.2 Standardization approach
      B.6 Standardization of thermal vacuum and cycling test
          conditions
          B.6.1 Evaluation of test requirements
          B.6.2 Standardization approach
      B.7 Conclusions
Annex C (normative) Test requirement specification - DRD
      C.1 Introduction
      C.2 Scope and applicability
          C.2.1 Scope
          C.2.2 Applicability
      C.3 References
          C.3.1 Glossary and dictionary
          C.3.2 Source document
      C.4 Terms and definitions and abbreviations
          C.4.1 Terms and definitions
          C.4.2 Abbreviations
      C.5 Description and purpose
      C.6 Application and interrelationship
      C.7 Test requirement specification preliminary elements
          C.7.1 Title
          C.7.2 Title page
          C.7.3 Contents list
          C.7.4 Foreword
          C.7.5 Introduction
      C.8 Content
          C.8.1 Scope and applicability
          C.8.2 References
          C.8.3 Definitions and abbreviations
          C.8.4 General test conditions and requirements
          C.8.5 Qualification testing
          C.8.6 Acceptance testing
          C.8.7 Protoflight testing
          C.8.8 Re-testing methodology
          C.8.9 GSE testing
Bibliography

This European Standard,a) specifies standard environmental and performance test requirements for a space system and its constituents;b) specifies the test requirements for products and systems that are generally applicable to all projects; c) specifies the documentation associated with testing activities;d) is applicable to all types and combinations of project, organization and product;e) is applicable to space systems and its constituents; and f) covers each stage of verification by testing, for a space system from development to post-landing.This European Standard does not specify acceptance criteria, specifications or procedures for any particular project or class of projects. In addition this Standard does not apply to software testing, hardware below equipment levels, nor covers the following:

Committee
CEN/BT
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy

Standards Relationship
I.S. EN 14824:2004 Identical
PN EN 14824 : 2004 Identical
UNI EN 14824 : 2004 Identical
BS EN 14824:2003 Identical
NEN EN 14824 : 2004 Identical
SN EN 14824 : 2004 Identical
NS EN 14824 : 1ED 2004 Identical
UNE-EN 14824:2003 Identical
NF EN 14824 : 2004 Identical
DIN EN 14824:2005-10 Identical
NBN EN 14824 : 2004 Identical

BS EN 14607-6:2004 Space engineering. Mechanical Pyrotechnics
BS EN 14607-5-1:2004 Space engineering. Mechanical Liquid and electric propulsion for spacecraft
DIN EN 14737-1:2004-12 SPACE ENGINEERING - GROUND SYSTEMS AND OPERATIONS - PART 1: PRINCIPLES AND REQUIREMENTS
I.S. EN 14607-6:2004 SPACE ENGINEERING - MECHANICAL - PART 6: PYROTECHNICS
I.S. EN 14607-5-1:2004 SPACE ENGINEERING - MECHANICAL - PART 5-1: LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT
I.S. EN 14737-1:2004 SPACE ENGINEERING - GROUND SYSTEMS AND OPERATIONS - PART 1: PRINCIPLES AND REQUIREMENTS
EN 14607-6:2004 Space engineering - Mechanical - Part 6: Pyrotechnics
EN 14607-5-1:2004 Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft
EN 14737-1:2004 Space engineering - Ground systems and operations - Part 1: Principles and requirements
BS EN 14737-1:2004 Space engineering. Ground systems and operations Principles and requirements

ISO 3744:2010 Acoustics Determination of sound power levels and sound energy levels of noise sources using sound pressure Engineering methods for an essentially free field over a reflecting plane
MIL-STD-1541 Revision A:1987 ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS
MIL-STD-1540 Revision D:1999 TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES
ISO 3740:2000 Acoustics Determination of sound power levels of noise sources Guidelines for the use of basic standards
EN 13701:2001 Space systems - Glossary of terms
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
MIL-STD-1833 Base Document:1989 TEST REQUIREMENTS FOR GROUND EQUIPMENT & ASSOCIATED COMPUTER SOFTWARE SUPPORTING SPACE VEHICLES
MIL-STD-462 Revision D:1993 MEASUREMENT OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS
EN 14725:2003 Space engineering - Verification

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