Name:
ISO 16127:2014 PDF
Published Date:
02/14/2014
Status:
[ Withdrawn ]
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.
| File Size : | 1 file , 450 KB |
| Note : | This product is unavailable in Ukraine, Russia, Belarus |
| Number of Pages : | 16 |
| Published : | 02/14/2014 |
| Same As : | ISO 16127:2014 |
