BS EN 16602 discusses adhesive bonding for spacecraft and launcher applications in space engineering.
BS EN 16602-70-16 is the sixteenth sub-part of the seventieth part of a multi-part series that specifies the generic verification for all types of adhesive bonding for space applications including evaluation phases.
BS EN 16602-70-16 covers all aspects of the adhesive bonding lifetime such as assembly, integration and testing, on-ground acceptance testing, storage, transport, prelaunch, launch, and in-flight environments.
Note: BS EN 16602-70-16 does not cover requirements for:
BS EN 16602-70-16 on adhesive bonding for spacecraft and launcher applications is applicable to:
Adhesives are widely used on spacecraft applications because of their several properties. All the adhesives used in spacecraft must be validated before the selection of appropriate adhesives and their behavior in the space environment be evaluated.
BS EN 16602-70-16 assists space agencies and industries in enabling the validation of adhesives and verification of the adhesive bonding process at an early stage of a program’s lifetime. BS EN 16602-70-16 provides you with the characteristics and properties of the adhesive to select the appropriate adhesive. BS EN 16602-70-16 also assists in the standardization of the verification processes for adhesives and adhesive bonding across the space industry.
By adopting BS EN 16602-70-16, you can demonstrate the reliability of your adhesives, and enhance value across the supply chain, to ultimately improve the operational efficiency of the end-product application.
EN 16602-70-16