Abstract
This International Standard specifies the common implementation process for meteoroid and debris environment models for risk assessment of spacecraft and launch vehicle orbital stages. This International Standard gives guidelines for the selection process of models for impact risk assessment and ensures the traceability of using models throughout the design phase of a spacecraft or launch vehicle orbital stage.
General information
-
Status: WithdrawnPublication date: 2012-11Stage: Withdrawal of International Standard [95.99]
-
Edition: 1Number of pages: 16
-
Technical Committee :ISO/TC 20/SC 14ICS :49.140
- RSS updates
Life cycle
-
Now
-
Revised by
PublishedISO 14200:2021