WEAPON SYSTEM 107A-2 PRODUCT ENGINEERING PROGRAM. COATED METALLIC THRUST CHAMBERS EXPANDABLE NOZZLES, COMBUSTION INSTABILITY SCALING CONCEPTS ABLATIVE THRUST CHAMBERS.
Abstract
Contents: Coated Metallic Thrust Chambers; Expandable nozzles; Combustion Instability Scaling Concepts; Ablative Thrust Chambers.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 15, 1964
- Accession Number
- AD0430285
Entities
Organizations
- Aerojet Rocketdyne Holdings