ISO 27852:2011 describes a process for the estimation of orbit lifetime for satellites, launch vehicles, upper stages and associated debris in LEO-crossing orbits.
ISO 27852:2011 also clarifies the modelling approaches and resources for solar and geomagnetic activity modelling; the resources for atmosphere model selection; and an approach for satellite ballistic coefficient estimation.
Status: WithdrawnPublication date: 2011-07
Edition: 1Number of pages: 28
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
- ICS :
- 49.140 Space systems and operations
ISO 27852:2011Stage: 95.99
Got a question?
Check out our FAQs
+41 22 749 08 88
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)
Keep up to date with ISO
Sign up to our newsletter for the latest news, views and product information.