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EN ISO 14620-1:2002

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space systems - Safety requirements - Part 1: System safety (ISO 14620-1:2002)

Superseded date

04-01-2018

Published date

12-01-2002

Foreword
Introduction
1 Scope
  1.1 General
  1.2 Field of application
  1.3 Tailoring
2 Normative references
3 Terms, definitions and abbreviated terms
  3.1 Terms and definitions
  3.2 Abbreviated terms
4 System safety programme
  4.1 Scope
  4.2 Safety organization
  4.3 Safety representative access and authority
  4.4 Safety risk management
  4.5 Project phases and safety review cycle
  4.6 Safety programme plan
  4.7 Safety certification
  4.8 Safety training
  4.9 Accident/incident reporting and investigation
  4.10 Safety documentation
5 Safety engineering
  5.1 Safety engineering policy
  5.2 Safety design principles
  5.3 Safety risk reduction and control
  5.4 Identification and control of safety critical functions
6 Safety analysis requirements and techniques
  6.1 General
  6.2 Assessment and allocation of requirements
  6.3 Safety analysis
  6.4 Specific safety analysis
  6.5 Supporting assessment and analysis
7 Safety verification
  7.1 General
  7.2 Tracking of hazards
  7.3 Safety verification methods
  7.4 Qualification of safety critical functions
  7.5 Hazard close-out
  7.6 Residual risk reduction
8 Operational safety
  8.1 Basic requirements
  8.2 Flight operations and mission control
  8.3 Ground operations
Bibliography

ISO 14620-1:2002 defines the safety programme and the technical safety requirements that are implemented in order to comply with the safety policy as defined in ISO 14300-2. It is intended to protect flight and ground personnel, the launch vehicle, associated payloads, ground support equipment, the general public, public and private property, and the environment from hazards associated with space systems. Launch site operations are described by ISO 14620-2.The safety policy is applied by implementing a system safety programme, supported by risk assessment, which can be summarized as follows: hazardous characteristics (system and environmental hazards) and functions with potentially hazardous failure effects are identified and progressively evaluated by iteratively performing systematic safety analyses; the potential hazardous consequences associated with the system characteristics and functional failures are subjected to a hazard reduction sequence whereby hazards are eliminated from the system design and operations, hazards are minimized, and hazard controls are applied and verified; the risks that remain after the application of a hazard elimination and reduction process are progressively assessed and subjected to risk assessment, in order to show compliance with safety targets, support design trades, identify and rank risk contributors, support apportionment of project resources for risk reduction, assess risk reduction progress, and support the safety and project decision-making process (e.g. waiver approval, residual risk acceptance); the adequacy of the hazard and risk control measures applied are formally verified in order to support safety validation and risk acceptance; safety compliance is assessed by the project and safety approval obtained from the relevant authorities.ISO 14620-1:2002 is applicable to all space projects where during any project phase there exists the potential for hazards to personnel or the general public, space flight systems, ground support equipment, facilities, public or private property, or the environment.The imposition of these requirements on the project suppliers' activities requires that the customer's project product assurance and safety organization also respond to these requirements in a manner which is commensurate with the project's safety criticality.When viewed from the perspective of a specific programme or project context, the requirements defined in ISO 14620-1:2002 should be tailored to match the genuine requirements of a particular profile and circumstances of a programme or project.

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

I.S. EN 14738:2004 SPACE PRODUCT ASSURANCE - HAZARD ANALYSIS
I.S. EN 13291-2:2004 SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 2: QUALITY ASSURANCE
I.S. EN 13291-3:2004 SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 3: MATERIALS, MECHANICAL PARTS AND PROCESSES
BS EN ISO 17666:2003 Space systems. Risk management
BS EN 14607-6:2004 Space engineering. Mechanical Pyrotechnics
BS EN 13291-3:2003 Space products assurance. General requirements Materials, mechanical parts and processes
BS EN 13291-2:2003 Space product assurance. General requirements Quality assurance
I.S. EN 14725:2004 SPACE ENGINEERING - VERIFICATION
DIN EN 14736:2004-09 SPACE PRODUCT ASSURANCE - QUALITY ASSURANCE FOR TEST CENTRES
EN 13291-3:2003 Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes
I.S. EN 14165:2004 SPACE ENGINEERING STANDARDS - FRACTURE CONTROL
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
DIN EN 13291-3:2005-03 SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 3: MATERIALS, MECHANICAL PARTS AND PROCESSES
I.S. EN 14736:2004 SPACE PRODUCT ASSURANCE - QUALITY ASSURANCE FOR TEST CENTRES
I.S. EN 14607-5-1:2004 SPACE ENGINEERING - MECHANICAL - PART 5-1: LIQUID AND ELECTRIC PROPULSION FOR SPACECRAFT
I.S. EN 14607-1:2004 SPACE ENGINEERING - MECHANICAL - PART 1: THERMAL CONTROL
I.S. EN 14737-1:2004 SPACE ENGINEERING - GROUND SYSTEMS AND OPERATIONS - PART 1: PRINCIPLES AND REQUIREMENTS
03/311010 DC : DRAFT JUNE 2003 EN 14725 - SPACE ENGINEERING - VERIFICATION
BS EN 14725:2003 Space engineering. Verification
BS EN 14738:2004 Space product assurance. Hazard analysis
ISO 17666:2016 Space systems — Risk management
BS EN 14165:2004 Space engineering standards. Fracture control
EN ISO 17666:2003 Space systems - Risk management (ISO 17666:2003)
EN 14736:2004 Space product assurance - Quality assurance for test centres
EN 14607-6:2004 Space engineering - Mechanical - Part 6: Pyrotechnics
EN 14725:2003 Space engineering - Verification
EN 14607-1:2004 Space engineering - Mechanical - Part 1: Thermal control
EN 14607-5-1:2004 Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft
EN 14738:2004 Space product assurance - Hazard analysis
EN 14737-1:2004 Space engineering - Ground systems and operations - Part 1: Principles and requirements
EN 14165:2004 Space engineering standards - Fracture control
I.S. EN ISO 17666:2003 SPACE SYSTEMS - RISK MANAGEMENT
03/311007 DC : DRAFT JUNE 2003 EN 13291-2 - SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 2: QUALITY ASSURANCE
BS EN 14607-1:2004 Space engineering. Mechanical Thermal control
BS EN 14736:2004 Space product assurance. Quality assurance for test centres
BS EN 14737-1:2004 Space engineering. Ground systems and operations Principles and requirements
EN 13291-2:2003 Space product assurance - General requirements - Part 2: Quality assurance
DIN EN 14165:2005-02 SPACE ENGINEERING STANDARDS - FRACTURE CONTROL
DIN EN 14738:2004-08 SPACE PRODUCT ASSURANCE - HAZARD ANALYSIS

ISO 14300-2:2011 Space systems — Programme management — Part 2: Product assurance
EN 13701:2001 Space systems - Glossary of terms
ISO 14300-1:2011 Space systems — Programme management — Part 1: Structuring of a project
ISO/IEC Guide 2:2004 Standardization and related activities General vocabulary
ISO 14620-2:2011 Space systems Safety requirements Part 2: Launch site operations
EN ISO 9000:2015 Quality management systems - Fundamentals and vocabulary (ISO 9000:2015)

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