Design and Test Requirements for Space Flight Pressurized Systems
Abstract
This Standard establishes the baseline requirements for the design, fabrication, assembly, installation, test, inspection, operation, and maintenance of pressure systems used in spacecraft and launch vehicles. This Standard is applicable to the procurement of pressurized hardware in space systems as a compliance document.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 26, 2014
- Accession Number
- ADA627256
Entities
People
- Mark J. Mueller
Organizations
- The Aerospace Corporation