BS ISO 14303:2002
Current
The latest, up-to-date edition.
Space systems. Launch-vehicle-to-spacecraft interfaces
Hardcopy , PDF
English
14-11-2002
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Foreword
Introduction
1 Scope
2 Terms and definitions
3 Symbols and abbreviated terms
4 Mechanical interfaces
5 Electrical interfaces
6 RF/electromagnetic interface
7 Mission performance
8 Induced environment and load limitations
9 Verification analysis and documentation
10 Verification tests
11 Spacecraft launch preparation operations
Annex A (informative) Usable envelopes
Annex B (informative) Physical interface presentations
Annex C (informative) Performance presentations
Annex D (informative) Environment presentations
Annex E (informative) Verification
Defines the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 99/708101 DC (11/2002)
|
| DocumentType |
Standard
|
| Pages |
62
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
This International Standard specifies the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces. Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique requirements.
| Standards | Relationship |
| ISO 14303:2002 | Identical |
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