DEVELOPMENT OF ALUMINUM BOBBIN SEALS FOR SEPARABLE CONNECTORS FOR ROCKET FLUID SYSTEMS
Abstract
During earlier research, it was shown that damage to the flanges of the 6061-T6 aluminum AFRPL connector could be prevented if the seal material was softer than the flange material by 20 points Brinell. Under Phase I of follow-on research, five methods of accomplishing this were studied: (1) soft coatings, (2) skin annealing, (3) softer aluminum alloys, (4) anodizing the flange, and (5) special aging of 6061-T6. The overaged 6061 aluminum for the seal was selected because of economic and technical reasons. Repeated-assembly, thermal-gradient, and stress-reversal-bending tests were conducted with helium-leakage rates below the limit of 7 x 10 to the minus 7th power atm cc/sec. Tentative specifications and standards were revised.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1967
- Accession Number
- AD0817843
Entities
People
- Bernard Goobich
- John R. Thompson
- Thomas M. Trainer
Organizations
- Battelle Memorial Institute