ISO 14622:2000
Space systems — Structural design — Loads and induced environment
Space systems — Structural design — Loads and induced environment
- Статус документа:
- Отменён
- Формат:
- Электронный (PDF)
- Количество страниц:
- 9
- Дата публикации:
- 21 декабря 2000 г.
- Издание:
- ISO IS 14622 edition 1 version 1
- ICS:
- 49.140
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.
Abstract
Overview
ISO 14622:2000 - "Space systems - Structural design - Loads and induced environment" defines principles for determining and the acting on a space flight vehicle and its components over their service life. The standard addresses probabilistic treatment of excitations, , corresponding , and lifecycle considerations (envelope, nominal and design lifetimes). It is produced by ISO/TC 20 (Aircraft and space vehicles), SC 14 (Space systems and operations).
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