BS ISO 16127:2014
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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Space systems. Prevention of break-up of unmanned spacecraft
Hardcopy , PDF
04-08-2022
English
28-02-2014
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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.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 12/30213836 DC. (02/2014)
|
| DocumentType |
Standard
|
| Pages |
20
|
| PublisherName |
British Standards Institution
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
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).
| 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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