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.

SDO:

ISO

Language:

English

ICS Codes:

49.140

Status:

Draft

Publish date:

1969-12-30

Standard Number:

ISO/DIS 14622