TUNGSTEN INSERT FIRING EVALUATION.
Abstract
The design and assembly of nozzles to be utilized in testing the first two W-2%Mo solid rocket nozzle inserts was completed. The nozzles will be fired on the Rocket Propulsion Laboratory solid rocket motor simulator. The inserts were closed die forged from stock that was vacuum centrifugal cast and extruded. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 31, 1964
- Accession Number
- AD0601966
Entities
People
- L. J. Stefan