DEVELOPMENT OF A SUPERSONIC TRANSPORT AIRCRAFT ENGINE - PHASE II-A.
Abstract
Contents: Analyses and Preliminary Design; Specifications; Compressor Development; Primary Combustion; Turbine Development; Augmentors; Exhaust System; Noise Reduction; Controls and Accessories; Bearing and Seal Development; Fuels; Lubricants; Inlets; Materials and Manufacturing Techniques; Operations and Economics; and Supporting Design Considerations.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 15, 1964
- Accession Number
- AD0370604
Entities
Organizations
- Pratt & Whitney