ISO/DIS 14622

Space systems — Structural design — Loads and induced environment

This International Standard defines the principles used to determine loads and the induced environment during the service life of a space flight vehicle and its components, taking account of the notions of probability, combined loads, corresponding safety factors and lifecycle.

OEN:

ISO

Langue:

English

Code(s) de l'ICS:

49.140

Statut:

Brouillon

Date de Publication:

1969-12-30

Numéro Standard:

ISO/DIS 14622