TECHNICAL PAPERS: Gas Turbines: Aircraft Engine

Integrated Vehicle Comparison of Turbo-Ramjet Engine and Pulsed Detonation Engine

[+] Author and Article Information
T. Kaemming

The Boeing Company, Mail Code S064-1042, St. Louis, MO 63166

J. Eng. Gas Turbines Power 125(1), 257-262 (Dec 27, 2002) (6 pages) doi:10.1115/1.1496116 History: Received December 01, 2000; Revised March 01, 2001; Online December 27, 2002
Copyright © 2003 by ASME
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Wortman, A., Othmer, P., and Rostafinski, W., 1992, “Detonation Duct Gas Generator Demonstration Program,” Paper No. AIAA-92-3174.
Bratkovich, T., Aarnio, M., and Bussing, T., 1997, “An Introduction to Pulse Detonation Rocket Engines (PDRE’s),” Paper No. AIAA-97-2742.


Grahic Jump Location
Engine specific fuel consumption comparison along baseline mission
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Tactical aircraft baseline mission sized weights
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Sized aircraft weights for alternate mission
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Total aircraft acquisition cost (baseline mission)
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Relative air vehicle acquisition costs (baseline mission)
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Relative total operating and support costs (baseline mission)
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Relative aircraft life cycle costs
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Pulse detonation technology engine architectures
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Tactical aircraft baseline mission
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Comparison of aircraft area distribution
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Engine thrust comparison along baseline mission




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