Accession Number:

AD0750984

Title:

Ducted-Fan Turbojet Engines (Review of Development Based on Foreign Publications),

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1972-08-29

Pagination or Media Count:

19.0

Abstract:

The author analyzes operating principles and the thermodynamic cycle of turbofan rocket engines. Given is a brief analysis of the present state of turbofan rocket engines abroad, an analysis of design characteristics of a series of power plants, and basic diagrams of engines, their merits and shortcomings. Indicated are also the advantages of turbofan rocket engines at high supersonic-flight M numbers in comparison with other types of engines, as well as the possible field of application of turbofan rocket engines. Author

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE