We use cookies to give you the best experience and to help improve our website
Find out what cookies we use and how to disable them
This document establishes general requirements for the application of fracture control technology to fracture-critical items (FCIs) fabricated from metallic, non-metallic or composite materials. It also establishes mechanical damage control requirements for mechanical-damage-critical items (MDCIs) fabricated from composite materials. These requirements, when implemented on a particular space system, can assure a high level of confidence in achieving safe operation and mission success.
The requirements set forth in this document are the minimum fracture control and mechanical damage control requirements for FCIs and MDCIs in general space systems, including launch vehicles, spacecraft and ground support equipment. With necessary modifications, these requirements may also be applicable to reusable launch vehicles (RLVs). This document is not applicable to the Shuttle and its payloads or the ISS and its equipment, since they already have a set of specific requirements suitable for their special applications.
This document is not applicable to processing detected defects.
Required form fields are indicated by an asterisk (*) character.
You are now following this standard. Weekly digest emails will be sent to update you on the following activities:
You can manage your follow preferences from your Account. Please check your mailbox junk folder if you don't receive the weekly email.
You have successfully unsubscribed from weekly updates for this standard.
Comment by: