NASA-STD-5019
FRACTURE CONTROL REQUIREMENTS FOR SPACEFLIGHT HARDWARE
| Organization: | NASA |
| Publication Date: | 7 January 2008 |
| Status: | inactive |
| Page Count: | 44 |
scope:
Purpose
Fracture control is implemented to reduce the risk of a catastrophic failure from a defect or damage. The intent of this standard is to provide fracture control requirements for spaceflight hardware. A variety of fracture control considerations and options are addressed, some of which may not be applicable to a given design. Information is provided to assist the user in the development of an effective Fracture Control Plan and other fracture control documentation.
Applicability
These requirements are not imposed on systems other than
human-rated spaceflight but may be tailored for use in specific
cases where it is prudent to do so, such as when national assets
are at risk. This standard may be cited in contract, program, and
other Agency documents as a technical requirement. Mandatory
requirements are indicated by the word "shall";
explanatory/guidance
Document History