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I.S. EN 14607-1:2004

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.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 ENGINEERING - MECHANICAL - PART 1: THERMAL CONTROL

Available format(s)

Hardcopy , PDF

Superseded date

10-11-2014

Language(s)

English

Published date

01-01-2004

Preview

For Harmonized Standards, check the EU site to confirm that the Standard is cited in the Official Journal.

Only cited Standards give presumption of conformance to New Approach Directives/Regulations.

Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
  3.1 Terms and definitions
  3.2 Definitions for unit internal thermal design
  3.3 Abbreviated terms
4 Requirements
  4.1 Mission
      4.1.1 General
      4.1.2 Ground and pre-launch
      4.1.3 Launch and ascent
      4.1.4 Planetary orbital phases
      4.1.5 Interplanetary phases
      4.1.6 Docking, docked and separation phases
      4.1.7 Descent, (re-)entry and landing
      4.1.8 Post-landing phases
  4.2 Performance
      4.2.1 General
      4.2.2 Temperatures
      4.2.3 Functionality
      4.2.4 Additional and other performance requirements
  4.3 Interfaces
      4.3.1 General
      4.3.2 Mechanical interface
      4.3.3 Electrical interface
      4.3.4 AOCS interface
      4.3.5 TM/TC interface
      4.3.6 OBDH and S/W interface
      4.3.7 Launcher interface
      4.3.8 GSE interface
  4.4 Design
      4.4.1 General
      4.4.2 Budgets
      4.4.3 Parts, materials and processes (PMP)
      4.4.4 EEE components
      4.4.5 Lifetime
      4.4.6 Predictability and testability
      4.4.7 Flexibility
      4.4.8 Accessibility
      4.4.9 Reliability
      4.4.10 Redundancy
      4.4.11 Interchangeability
      4.4.12 Maintenance
      4.4.13 Cleanliness
      4.4.14 Safety
      4.4.15 Availability
  4.5 Verification
      4.5.1 General
      4.5.2 Review of design
      4.5.3 Verification by similarity
      4.5.4 Verification by inspection
      4.5.5 Verification by analysis
      4.5.6 Verification by test
      4.5.7 Thermal Balance (TB) test
  4.6 Production and manufacturing
      4.6.1 General
      4.6.2 Manufacturing process
      4.6.3 Manufacturing drawings
      4.6.4 Quality management
      4.6.5 Cleanliness
      4.6.6 Procurement
      4.6.7 Tooling
      4.6.8 Integration
      4.6.9 Marking
      4.6.10 Packaging, handling, transportation
      4.6.11 Storage
      4.6.12 Repair
      4.6.13 In-service requirements
  4.7 Product assurance
  4.8 Deliverables
      4.8.1 General
      4.8.2 Hardware
      4.8.3 Documentation
  4.9 Use standard to define project requirements
Annex A (normative) Development approach
  A.1 Uncertainties
      A.1.1 Uncertainty philosophy
      A.1.2 Sources for temperature uncertainties
      A.1.3 Sensitivity analysis and temperature uncertainty
  A.2 Margins
  A.3 Test approach and test success criteria
      A.3.1 Test approach
      A.3.2 Test success criteria
  A.4 Correlation approach and correlation success criteria
      A.4.1 General
      A.4.2 Temperature level criteria
      A.4.3 Standard deviation criteria
      A.4.4 Individual unit success criteria
  A.5 Analysis approach
      A.5.1 Objectives of thermal analysis
      A.5.2 Thermal analysis methods
      A.5.3 Interfaces and deliverables
      A.5.4 Quality
Annex B (normative) Cryogenic temperature range
  B.1 Applicability
      B.1.1 General
      B.1.2 Cryogenic definitions (exceptions)
  B.2 Complementary terminology for the cryogenic
      temperature range
  B.3 Applicability matrix
Annex C (normative) High temperature range
  C.1 Applicability
  C.2 Complementary terminology for the high temperature
      range
  C.3 Applicability matrix
Annex D (informative) TCS development methodology
  D.1 Conventional temperature range
      D.1.1 General
      D.1.2 First stage (preliminary) configuration
      D.1.3 Final thermal design
      D.1.4 Reason for thermal analyses
      D.1.5 Typical parameter inaccuracies
  D.2 Cryogenic temperature range
      D.2.1 General
      D.2.2 Reason for thermal analyses
      D.2.3 Typical parameter inaccuracies
Bibliography

Provides the requirements for the definition, analysis, design, manufacture, verification and in-service operation of thermal control subsystems of spacecraft and other space products.

DocumentType
Standard
Pages
54
PublisherName
National Standards Authority of Ireland
Status
Superseded
SupersededBy

Standards Relationship
NF EN 14607-1 : 2004 Identical
NBN EN 14607-1 : 2004 Identical
UNI EN 14607-1 : 2005 Identical
BS EN 14607-1:2004 Identical
NEN EN 14607-1 : 2004 Identical
NS EN 14607-1 : 1ED 2004 Identical
DIN EN 14607-1:2006-12 Identical
EN 14607-1:2004 Identical

EN 13290-5:2001 Space project management - General requirements - Part 5: Configuration management
EN 13291-3:2003 Space product assurance - General requirements - Part 3: Materials, mechanical parts and processes
EN 13701:2001 Space systems - Glossary of terms
ISO 14620-1:2002 Space systems Safety requirements Part 1: System safety
EN ISO 14620-1:2002 Space systems - Safety requirements - Part 1: System safety (ISO 14620-1:2002)
ISO 128:1982 Technical drawings — General principles of presentation
EN 13291-2:2003 Space product assurance - General requirements - Part 2: Quality assurance
EN 14725:2003 Space engineering - Verification

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