Accession Number:

ADD009476

Title:

Gas Turbine Cycle Providing a High Pressure Efflux.

Descriptive Note:

Patent,

Corporate Author:

DEPARTMENT OF THE NAVY WASHINGTON DC

Personal Author(s):

Report Date:

1968-05-14

Pagination or Media Count:

3.0

Abstract:

This invention relates to a system for developing propulsive thrust by the reaction of a flow of energized fluid and in particular is concerned with a gas turbine cycle of operation for developing the propulsive thrust.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE