Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

30-04-2012

Publisher

British Standards Institution

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.

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.

Committee	ACE/68
DevelopmentNote	Supersedes 10/30240189 DC. (04/2012)
DocumentType	Standard
Pages	26
PublisherName	British Standards Institution
Status	Current
Supersedes	10/30240189 DC : 0

Standards	Relationship
ISO 26869:2012	Identical

ISO 15863:2003

Space systems Spacecraft-to-launch-vehicle interface control document

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BS ISO 26869:2012

Space systems. Small-auxiliary-spacecraft (SASC) to-launch-vehicle interface control document

Table of Contents

Abstract

Scope

General Product Information

International Equivalents

Standards Referencing This Book

Category

Subcategory