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.
Harpoon Expendable Turbojet Model XJ401-GA-400
1973
354 pages
Report
Keine Angabe
Englisch
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