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ISO 14620-1:2002
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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Space systems Safety requirements Part 1: System safety
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
27-02-2019
English
25-11-2002
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.
DevelopmentNote |
DRAFT ISO/DIS 14620-1 is also available for this standard. (06/2017)
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DocumentType |
Standard
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Pages |
37
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PublisherName |
International Organization for Standardization
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Status |
Withdrawn
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SupersededBy |
Standards | Relationship |
NBR ISO 14620-1 : 2009 | Identical |
UNE-EN ISO 14620-1:2002 | Identical |
NF EN ISO 14620-1 : 2004 | Identical |
NBN EN ISO 14620-1 : 2003 | Identical |
NS EN ISO 14620-1 : 1ED 2003 | Identical |
I.S. EN ISO 14620-1:2002 | Identical |
PN EN ISO 14620-1 : 2003 | Identical |
SN EN ISO 14620-1 : 2003 | Identical |
UNI EN ISO 14620-1 : 2003 | Identical |
BS EN ISO 14620-1:2002 | Identical |
EN ISO 14620-1:2002 | Identical |
DIN EN ISO 14620-1:2005-06 | Identical |
15/30303532 DC : 0 | BS ISO 17770 - SPACE SYSTEMS - CUBE SATELLITES (CUBESATS) |
08/30150852 DC : 0 | BS ISO 14620-2 - SPACE SYSTEMS SAFETY REQUIREMENTS - PART 2: LAUNCH SITE OPERATIONS |
BS ISO 17770:2017 | Space systems. Cube satellites (CubeSats) |
07/30150339 DC : 0 | BS ISO 27025 - SPACE SYSTEMS - PROGRAMME MANAGEMENT - QUALITY ASSURANCE REQUIREMENTS |
BS ISO 19683:2017 | Space systems. Design qualification and acceptance tests of small spacecraft and units |
ISO 19683:2017 | Space systems — Design qualification and acceptance tests of small spacecraft and units |
BS EN ISO 17666:2003 | Space systems. Risk management |
BS EN 14607-6:2004 | Space engineering. Mechanical Pyrotechnics |
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 |
PD ISO/TS 18667:2018 | Space systems. Capability-based Safety, Dependability, and Quality Assurance (SD&QA) programme management |
BS ISO 27025:2010 | Space systems. Programme management. Quality assurance requirements |
ISO/IEC 15026-1:2013 | Systems and software engineering Systems and software assurance Part 1: Concepts and vocabulary |
BS ISO 14300-1:2011 | Space systems. Programme management Structuring of a project |
ISO 14620-2:2011 | Space systems Safety requirements Part 2: Launch site operations |
ISO 27025:2010 | Space systems — Programme management — Quality assurance requirements |
CSA ISO/IEC 15026-1 : 2015 | SYSTEMS AND SOFTWARE ENGINEERING - SYSTEMS AND SOFTWARE ASSURANCE - PART 1: CONCEPTS AND VOCABULARY |
ISO 14625:2007 | Space systems — Ground support equipment for use at launch, landing or retrieval sites — General requirements |
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 |
02/709705 DC : DRAFT AUG 2002 | BS ISO 15865 - SPACE SYSTEMS - QUALIFICATION ASSESSMENT |
I.S. EN 14098:2002 | SPACE PRODUCT ASSURANCE - THERMAL CYCLING TEST FOR THE SCREENING OF SPACE MATERIALS AND PROCESSES |
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 |
10/30197293 DC : 0 | BS ISO 14300-2 - SPACE SYSTEMS - PROGRAMME MANAGEMENT - PART 2: PRODUCT ASSURANCE |
BS ISO 14620-2:2011 | Space systems. Safety requirements Launch site operations |
ISO/TS 18667:2018 | Space systems — Capability-based Safety, Dependability, and Quality Assurance (SD&QA) programme management |
ISO 14620-3:2005 | Space systems Safety requirements Part 3: Flight safety systems |
ISO 14950:2004 | Space systems — Unmanned spacecraft operability |
ISO 14619:2003 | Space systems — Space experiments — General requirements |
ISO 14300-2:2011 | Space systems — Programme management — Part 2: Product assurance |
EN 14099:2001 | Space product assurance - Measurement of the peel and pull-off strength of coatings and finishes using pressure-sensitive tapes |
EN 14089:2002 | Space product assurance - The control of limited shelf-life materials |
BS ISO 18322:2017 | Space systems. General management requirements for space test centres |
I.S. EN 14737-1:2004 | SPACE ENGINEERING - GROUND SYSTEMS AND OPERATIONS - PART 1: PRINCIPLES AND REQUIREMENTS |
I.S. EN 14089:2002 | SPACE PRODUCT ASSURANCE - THE CONTROL OF LIMITED SHELF-LIFE MATERIALS |
BS ISO/IEC 15026-1:2013 | Systems and software engineering. Systems and software assurance Concepts and vocabulary |
ISO 24917:2010 | Space systems General test requirements for launch vehicles |
BS ISO 14625:2007 | Space systems. Ground support equipment for use at launch, landing or retrieval sites. General requirements |
BS ISO 14300-2:2011 | Space systems. Programme management Product assurance |
17/30318744 DC : 0 | BS ISO 20188 - SPACE SYSTEMS - PRODUCT ASSURANCE REQUIREMENTS FOR COMMERCIAL SATELLITES |
ISO 20188:2018 | Space systems — Product assurance requirements for commercial satellites |
BS ISO 27875 : 2010 | SPACE SYSTEMS - RE-ENTRY RISK MANAGEMENT FOR UNMANNED SPACECRAFT AND LAUNCH VEHICLE ORBITAL STAGES |
ISO 27875:2010 | Space systems Re-entry risk management for unmanned spacecraft and launch vehicle orbital stages |
ISO 18322:2017 | Space systems — General management requirements for space test centres |
ISO 14300-1:2011 | Space systems — Programme management — Part 1: Structuring of a project |
BS EN 14607-1:2004 | Space engineering. Mechanical Thermal control |
BS EN 14089:2002 | Space product assurance. The control of limited shelf-life materials |
03/311008 DC : DRAFT JUNE 2003 | EN 14165 - SPACE ENGINEERING STANDARDS - FRACTURE CONTROL |
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 14099:2001 | Space product assurance. Measurement of the peel and pull-off strength of coatings and finishes using pressure-sensitive tapes |
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 14098:2001 | Space product assurance - Thermal cycling test for the screening of space materials and processes |
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 14099:2002 | SPACE PRODUCT ASSURANCE - MEASUREMENT OF THE PEEL AND PULL-OFF STRENGTH OF COATINGS AND FINISHES USING PRESSURE-SENSITIVE TAPES |
08/30191606 DC : 0 | BS ISO 24917 - SPACE SYSTEMS - GENERAL TEST REQUIREMENTS FOR LAUNCH VEHICLES |
03/311007 DC : DRAFT JUNE 2003 | EN 13291-2 - SPACE PRODUCT ASSURANCE - GENERAL REQUIREMENTS - PART 2: QUALITY ASSURANCE |
09/30192797 DC : 0 | BS ISO 27875 - SPACE SYSTEMS - RE-ENTRY RISK MANAGEMENT FOR UNMANNED SPACECRAFT AND LAUNCH VEHICLE ORBITAL STAGES |
BS ISO 24917:2010 | Space systems. General test requirements for launch vehicles |
BS ISO 14619:2003 | Space systems. Space experiments. General requirements |
BS ISO 14950:2004 | Space systems. Unmanned spacecraft operability |
16/30302535 DC : 0 | BS ISO 19683 - SPACE SYSTEMS - DESIGN QUALIFICATION AND ACCEPTANCE TESTS OF SMALL SPACECRAFT AND UNITS |
03/301398 DC : DRAFT JAN 2003 | EN 14607-6 - SPACE ENGINEERING - MECHANICAL - PART 6: PYROTECHNICS |
ISO 17770:2017 | Space systems — Cube satellites (CubeSats) |
IEEE/ISO/IEC 15026-1-2014 | IEEE Standard Adoption of ISO/IEC 15026-1--Systems and Software Engineering--Systems and Software Assurance--Part 1: Concepts and Vocabulary |
BS EN 14098:2001 | Space product assurance. Thermal cycling test for the screening of space materials and processes |
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 |
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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