BS EN 16603-10 discusses standards for space engineering.
BS EN 16603‑32‑10 is part of a series of documents that specifies the Factors Of Safety (FOS), design Factor and additional factors to be used for the dimensioning and design verification of spaceflight hardware including qualification and acceptance tests.
Note: BS EN 16603‑32‑10 does not address factors of safety for re-usable launch vehicles and man-rated commercial spacecraft.
BS EN 16603-32-10 on space engineering is applicable to:
BS EN 16603-32-10 helps spacecraft manufacturers in the dimensions and design verification of spacelight hardware.
BS EN 16603-32-10 provides you with an adequate level of mechanical reliability for spaceflight hardware.
By adopting BS EN 16603-32-10, manufacturers can demonstrate the reliability of their spacecraft and space products and build trust in its use throughout the space engineering supply chain.
EN 16603-32-10