Abstract

 Preview

ISO 27852:2016 describes a process for the estimation of orbit lifetime for spacecraft, launch vehicles, upper stages and associated debris in LEO-crossing orbits.

It also clarifies the following:

a) modelling approaches and resources for solar and geomagnetic activity modelling;

b) resources for atmosphere model selection;

c) approaches for spacecraft ballistic coefficient estimation.


General information 

  • Status
     :  Published
    Publication date
     : 2016-07
  • Edition
     : 2
    Number of pages
     : 43
  • Technical Committee
     : ISO/TC 20/SC 14 Space systems and operations
  • ICS
     :
    49.140 Space systems and operations

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal:

9
Industry, Innovation and Infrastructure

Buy this standard

Format Language
PDF + ePub
Paper
  • CHF166

Life cycle


Got a question?

Check out our FAQs

Customer care
+41 22 749 08 88

Opening hours:
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.

  2. Store
  3. Standards catalogue
  4. TC
  5. ISO/TC 20/SC 14
  6. ISO 27852:2016