Abstract

The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia. The general concepts defined are applicable to the atmospheric flight phase.


General information 

  • Status
     :  Withdrawn
    Publication date
     : 1992-06
  • Edition
     : 1
    Number of pages
     : 8
  • Technical Committee
     : ISO/TC 20/SC 8 Aerospace terminology
  • ICS
     :
    01.060 Quantities and units
    49.020 Aircraft and space vehicles in general

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal:

9
Industry, Innovation and Infrastructure

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. ICS
  5. 01
  6. 01.060
  7. ISO 1151-8:1992