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BS ISO 16127:2014

BS ISO 16127:2014

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by
superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space systems. Prevention of break-up of unmanned spacecraft

Available format(s)

Hardcopy , PDF

Superseded date

08-04-2022

Language(s)

English

Published date

02-28-2014

Publisher

British Standards Institution

Foreword
Introduction
1 Scope
2 Normative references
3 Terms and definitions
4 Implementation
5 Stored energy sources
Annex A (informative) - Procedure for estimating
         break-up probability
Bibliography

Specifies the requirements to reduce the risk of in-orbit break-up of unmanned spacecraft, both during and after their operational lives.

This International Standard defines the requirements to reduce the risk of in-orbit break-up of unmanned spacecraft, both during and after their operational lives. The aim would be met by reducing the possibility of a break-up caused by an unplanned internally caused event and by depleting to a safe level all the sources of stored energy at the end of a spacecraft’s life. This International Standard is designed for use in planning, verifying, and implementing the prevention of break-up of a spacecraft.

This International Standard applies only to unmanned spacecraft operating in Earth orbit. It does not apply to manned space vehicles or launch vehicle orbital stages. Additionally, it does not cover nuclear power sources within spacecraft.

This International Standard is not applicable to fragmentation as a result of external particle impacts (which includes fragmentations triggered by external particle impact but powered by internal energy sources).

Committee
ACE/68
DevelopmentNote
Supersedes 12/30213836 DC. (02/2014)
DocumentType
Standard
Pages
20
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

Standards Relationship
ISO 16127:2014 Identical

ISO 24638:2008 Space systems Pressure components and pressure system integration
ISO 10795:2011 Space systems Programme management and quality Vocabulary
MIL-STD-1522 Revision A:1984 STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS
ISO 24113:2011 Space systems Space debris mitigation requirements
ISO 21347:2005 Space systems — Fracture and damage control
ISO 17666:2016 Space systems — Risk management
ISO 14623:2003 Space systems - Pressure vessels and pressurized structures Design and operation

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Hardcopy - English
PDF - English
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