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EN 16603-10-04:2015

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Space engineering - Space environment

Superseded date

17-09-2021

Superseded by

EN 16603-10-04:2021

Published date

28-01-2015

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Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 Gravity
5 Geomagnetic fields
6 Natural electromagnetic radiation and indices
7 Neutral atmospheres
8 Plasmas
9 Energetic particle radiation
10 Space debris and meteoroids
11 Contamination
Annex A (normative) - Natural electromagnetic radiation
        and indices
Annex B (normative) - Energetic particle radiation
Annex C (normative) - Space debris and meteoroids
Annex D (informative) - Gravitation
Annex E (informative) - Geomagnetic fields
Annex F (informative) - Natural electromagnetic radiation
        and indices
Annex G (informative) - Neutral atmospheres
Annex H (informative) - Plasmas
Annex I (informative) - Energetic particle radiation
Annex J (informative) - Space debris and meteoroids
Annex K (informative) - Contamination modelling and tools
Bibliography

This standard applies to all product types which exist or operate in space and defines the natural environment for all space regimes. It also defines general models and rules for determining the local induced environment.Project-specific or project-class-specific acceptance criteria, analysis methods or procedures are not defined.The natural space environment of a given item is that set of environmental conditions defined by the external physical world for the given mission (e.g. atmosphere, meteoroids and energetic particle radiation). The induced space environment is that set of environmental conditions created or modified by the presence or operation of the item and its mission (e.g. contamination, secondary radiations and spacecraft charging). The space environment also contains elements which are induced by the execution of other space activities (e.g. debris and contamination).This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.

Committee
CEN/CLC/JTC 5
DevelopmentNote
Supersedes EN 14092. (02/2015)
DocumentType
Standard
PublisherName
Comite Europeen de Normalisation
Status
Superseded
SupersededBy
Supersedes

BS EN 16602-60-15:2014 Space product assurance. Radiation hardness assurance. EEE components
I.S. EN 16602-70-01:2014 SPACE PRODUCT ASSURANCE - CLEANLINESS AND CONTAMINATION CONTROL
BS EN 16603-35:2014 Space engineering. Propulsion general requirements
BS EN 16602-70-06:2014 Space product assurance. Particle and UV radiation testing for space materials
I.S. EN 16602-60:2015 SPACE PRODUCT ASSURANCE - ELECTRICAL, ELECTRONIC AND ELECTROMECHANICAL (EEE) COMPONENTS
BS EN 16603-31:2014 Space engineering. Thermal control general requirements
I.S. EN 16603-35:2014 SPACE ENGINEERING - PROPULSION GENERAL REQUIREMENTS
BS EN 16603-10-12:2014 Space engineering. Method for the calculation of radiation received and its effects, and a policy for design margins
UNI EN 16603-20-06 : 2014 SPACE ENGINEERING - SPACECRAFT CHARGING
EN 16603-10:2018 Space engineering - System engineering general requirements
EN 16603-20-06:2014 Space engineering - Spacecraft charging
EN 16602-60:2015 Space product assurance - Electrical, electronic and electromechanical (EEE) components
EN 16603-10-12:2014 Space engineering - Method for the calculation of radiation received and its effects, and a policy for design margins
BS EN 16603-20-06:2014 Space engineering. Spacecraft charging
BS EN 16602-60:2015 Space product assurance. Electrical, electronic and electromechanical (EEE) components
I.S. EN 16603-10:2018 SPACE ENGINEERING - SYSTEM ENGINEERING GENERAL REQUIREMENTS
BS EN 16602-70-01:2014 Space product assurance. Cleanliness and contamination control
I.S. EN 16602-60-15:2014 SPACE PRODUCT ASSURANCE - RADIATION HARDNESS ASSURANCE - EEE COMPONENTS
I.S. EN 16603-10-12:2014 SPACE ENGINEERING - METHOD FOR THE CALCULATION OF RADIATION RECEIVED AND ITS EFFECTS, AND A POLICY FOR DESIGN MARGINS
I.S. EN 16603-31:2014 SPACE ENGINEERING - THERMAL CONTROL GENERAL REQUIREMENTS
EN 16603-35:2014 Space engineering - Propulsion general requirements
EN 16602-60-15:2014 Space product assurance - Radiation hardness assurance - EEE components
EN 16603-31:2014 Space engineering - Thermal control general requirements
EN 16602-70-06:2014 Space product assurance - Particle and UV radiation testing for space materials
EN 16602-70-01:2014 Space product assurance - Cleanliness and contamination control
I.S. EN 16602-70-06:2014 SPACE PRODUCT ASSURANCE - PARTICLE AND UV RADIATION TESTING FOR SPACE MATERIALS
UNI EN 16603-10-12 : 2014 SPACE ENGINEERING - METHOD FOR THE CALCULATION OF RADIATION RECEIVED AND ITS EFFECTS, AND A POLICY FOR DESIGN MARGINS
I.S. EN 16603-20-06:2014 SPACE ENGINEERING - SPACECRAFT CHARGING

MIL-STD-1809 Base Document:1991 SPACE ENVIRONMENT FOR USAF SPACE VEHICLES
ASTM E 595 : 2015 : REDLINE Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment
ISO 5878:1982 Reference atmospheres for aerospace use
ISO 2533:1975 Standard Atmosphere
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16602-70-01:2014 Space product assurance - Cleanliness and contamination control
EN 16603-10-12:2014 Space engineering - Method for the calculation of radiation received and its effects, and a policy for design margins
EN 16603-20-06:2014 Space engineering - Spacecraft charging

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