Accession Number:

AD0857455

Title:

Suggested Specification for a Lift Fan Propulsion System

Descriptive Note:

Final technical rept. 1 Jul 1965-1 Mar 1966

Corporate Author:

RYAN AERONAUTICAL CO SAN DIEGO CA

Personal Author(s):

Report Date:

1969-05-01

Pagination or Media Count:

49.0

Abstract:

The report presents propulsion system component design requirements believed to be necessary for successful development of operational lift fan aircraft. The work was done for the purpose of identifying lift fan airframe and propulsion system performance and installation interfaces. The requirements presented in the report reflect experience gained from the XV-5A lift fan aircraft flight test program.

Subject Categories:

  • VSTOL
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE