Impacts of mission-related requirements on design of the J402-CA-400 missile propulsion turbojet engine are reviewed. Small-engine cost scaling rationale is presented in relation to engine thrust and functional requirements. The application of current casting technology toward achieving low cost is reviewed.
Turbine Powerplants for Missiles - Cost Improvement Requirements
Sae Technical Papers
National Air Transportation Meeting ; 1973
1973-02-01
Conference paper
English
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