ISO 16127:2014 PDF
Space systems — Prevention of break-up of unmanned spacecraft
Title (English):
ISO 16127:2014
Space systems — Prevention of break-up of unmanned spacecraft
- Document status:
- Withdrawn
- Format:
- Electronic (PDF)
- Number of pages:
- 9
- Publication date:
- February 13, 2014
- Edition:
- ISO IS 16127 edition 1 version 1
- ICS:
- 49.140
Description (English):
ISO 16127:2014 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. ISO 16127:2014 is designed for use in planning, verifying and implementing the prevention of break-up of a spacecraft. ISO 16127:2014 applies only to unmanned spacecraft operating in Earth orbit.
Technical details
- Technical committee
- ISO/TC 20/SC 14 - Space systems and operations
- SKU
- ISO 16127:2014
