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Navy Development of Low-Cost Supersonic Turbojet Engines
ISSN: 0148-7191, e-ISSN: 2688-3627
Published February 01, 1973 by SAE International in United States
Annotation ability available
This paper is a review of a Naval Air Systems Command program for exploratory development of a low-cost supersonic turbine engine. Design constraints, performance requirements, estimated engine costs, and latest program results are presented. Briefly described, the engine is 14 in in diameter, 44 in in length, produces 2300 lb thrust at Mach 1.5, sea level, (approximately 1600 lb, sea level static), and is estimated to cost $7000-11,000 in production.
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CitationWalker, D., "Navy Development of Low-Cost Supersonic Turbojet Engines," SAE Technical Paper 730362, 1973, https://doi.org/10.4271/730362.
- AiResearch Manufacturing Co. of Arizona “Low Cost Ordnance Quality Expendable Turbine Engine Design.” Final Report to the Naval Weapons Center under Contract No. N00123-72-C-0253, NWC TP 5334 November 1972
- Curtiss-Wright Corp. “Low Cost, Ordnance Quality Expendable Turbine Engine Design.” Final Report to the Naval Weapons Center under Contract No. N00123-72-C-0731, NWC TP 5335 November 1972