EN 16603-10-04:2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
17-09-2021
28-01-2015
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Superseded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 |
Standards | Relationship |
UNE-EN 16603-10-04:2015 | Identical |
NS EN 16603-10-04 : 2015 | Identical |
UNI CEI EN 16603-10-04 : 2015 | Identical |
PN EN 16603-10-04 : 2015 | Identical |
DIN EN 16603-10-04:2015-05 | Identical |
BS EN 16603-10-04:2015 | Identical |
NF EN 16603-10-04 : 2016 | Identical |
NBN EN 16603-10-04 : 2015 | Identical |
CEI UNI EN 16603-10-04 : 1ED 2016 | Identical |
I.S. EN 16603-10-04:2015 | Identical |
NEN EN 16603-10-04 : 2015 | Identical |
ONORM EN 16603-10-04 : 2015 | Identical |
PNE-FprEN 16603-10 -04 | Identical |
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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