Concept of a Synergetic Air-Breathing Engine for Hypersonic Flight
Abstract
This report results from a contract tasking Central Aerohydrodynamics Institute as follows: The contractor will investigate an analysis of main characteristics of turbo-compressor engine new design for hypersonic flight as per his 8 Mar 95 proposal.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1997
- Accession Number
- ADA329583
Entities
People
- Yury Lobanovsky