This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Turbine Powerplants for Missiles - Cost Improvement Requirements
Annotation ability available
Sector:
Language:
English
Abstract
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.
Recommended Content
Technical Paper | Large Lightweight Turbojet Engines |
Technical Paper | Design Features for Maintainability in the Pratt and Whitney Aircraft J9D Gas Turbine Engine |
Technical Paper | GE4 SUPERSONIC TRANSPORT ENGINE-DEVELOPMENT PROGRESS AND STATUS |
Authors
Citation
Kidd, W., "Turbine Powerplants for Missiles - Cost Improvement Requirements," SAE Technical Paper 730364, 1973, https://doi.org/10.4271/730364.Also In
References
- Maskey H. C. Marsh F. X. “The Annular Combustion Chamber with Centrifugal Fuel Injection.” Paper 444C SAE Automotive Engineering Congress Detroit January 1962
- Burdette G. N. Couch D. H. Burgner G. R. Walker D. W. “High Density Air Breather Fuels.” Air Breathing Propulsion III Session of the 1972 JANNAF 8th Propulsion Joint Specialists Conference New Orleans November 1972
- Brennan T. J. Taylor R. N. Steinert A. G. “Cost Estimating Techniques for Advanced Technology Engines.” Paper 700271 SAE National Air Transportation Meeting New York April 1970
- Air Force Aero Propulsion Laboratory Technical Report AFAPL-TR-71-103 December 1971