Accession Number:

AD0766145

Title:

Harpoon Expendable Turbojet Model XJ401-GA-400

Descriptive Note:

Final rept. 30 Jun 1971-13 Apr 1973 on Phase 2

Corporate Author:

AIRESEARCH MFG CO OF ARIZONA PHOENIX

Personal Author(s):

Report Date:

1973-04-25

Pagination or Media Count:

335.0

Abstract:

The report documents Phase 2 of the development of a turbojet propulsion system for the Harpoon missile and covers the period from 30 June 1971 through 13 April 1973. The objectives of the Phase 2 development program were Design, fabrication and development of engine suitable for wind tunnel and flight testing Delivery of above engines to the weapons system contractor and Technical liaison with the weapons system contractor, including systems test support.

Subject Categories:

  • Air- and Space-Launched Guided Missiles
  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE