Alternative Processing to Electrodeposition to form Thrust Chamber Structural Jackets
Abstract
Identify, demonstrate, and develop a method of forming a liquid rocket engine thrust chamber structural jacket that is less expensive than electrodeposition and capable of applying nanostructured materials. Document and demonstrate cost and/or weight advantages over conventional electrodeposition of nickel.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 28, 2002
- Accession Number
- ADB282731
Entities
People
- J. S. Shelley
Organizations
- Air Force Research Laboratory