BS ISO 26869:2012
Current
The latest, up-to-date edition.
Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document
Hardcopy , PDF
English
30-04-2012
Foreword
Introduction
1 Scope
2 Normative reference
3 Terms, definitions and abbreviated terms
4 Applicable and reference documentation
5 SASC mission characteristics
6 Mechanical interface
7 Electrical interfaces
8 Radio frequency and electromagnetic interface
9 LV and SASC mission characteristics
10 Induced environment
11 Verification tests
12 Launch-range operation
Gives small auxiliary spacecraft (SASC) and launch vehicle (LV) organizations with basic rules for writing an interface control document (ICD), and a general format for the document's presentation, when the SASC has an interface (I/F) only with the LV.
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 10/30240189 DC. (04/2012)
|
DocumentType |
Standard
|
Pages |
26
|
PublisherName |
British Standards Institution
|
Status |
Current
|
Supersedes |
This International Standard provides small auxiliary spacecraft (SASC) and launch vehicle (LV) organizations with basic rules for writing an interface control document (ICD), and a general format for the document\'s presentation, when the SASC has an interface (I/F) only with the LV.
It is applicable to the necessary ICD items and restrictions peculiar to SASCs, these spacecraft being as defined in the contract between the launch agency and the contractor.
The payload area covered by this International Standard is limited to SASC.
NOTE SASCs have minor priorities with respect to the main spacecraft.
Standards | Relationship |
ISO 26869:2012 | Identical |
ISO 15863:2003 | Space systems Spacecraft-to-launch-vehicle interface control document |
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