Harpoon Expendable Turbojet Model XJ401-GA-400
Final rept. 30 Jun 1971-13 Apr 1973 on Phase 2
AIRESEARCH MFG CO OF ARIZONA PHOENIX
Pagination or Media Count:
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.
- Air- and Space-Launched Guided Missiles
- Jet and Gas Turbine Engines