Logo
Login Sign Up
Current Revision

BSI BS ISO 16127:2014

Space systems. Prevention of break-up of unmanned spacecraft
Best Price Guarantee
Instant

$222.36

2-5 Days

$222.36

SAVE 10%

$400.25


Sub Total (1 Item(s))

$ 0.00

Estimated Shipping

$ 0.00

Total (Pre-Tax)

$ 0.00


View in Library
or
British Standards Institution Logo

BSI BS ISO 16127:2014

Space systems. Prevention of break-up of unmanned spacecraft

PUBLISH DATE 2014
PAGES 20
BSI BS ISO 16127:2014

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).

SDO BSI: British Standards Institution
Document Number ISO 16127
Publication Date Feb. 28, 2014
Language en - English
Page Count
Revision Level
Supercedes
Committee ACE/68
Loading...

Failed to load document history.

Publish Date Document Id Type View