Accession Number:

ADA329583

Title:

Concept of a Synergetic Air-Breathing Engine for Hypersonic Flight

Descriptive Note:

Final rept.

Corporate Author:

CENTRAL AERODYNAMIC INST MOSCOW (RUSSIA)

Personal Author(s):

Report Date:

1997-08-01

Pagination or Media Count:

29.0

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.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE