Accession Number:

ADA460539

Title:

A Hydrocarbon Fuel Flash Vaporization System for a Pulsed Detonation Engine

Descriptive Note:

Journal article (preprint)

Corporate Author:

AIR FORCE RESEARCH LAB EGLIN AFB FL MUNITIONS DIRECTORATE

Personal Author(s):

• Tucker, K. C.
• King, Paul I.
• Schauer, Frederick R.

Report Date:

2006-12-01

Pagination or Media Count:

29.0

Abstract:

Practical operation of pulsed detonation propulsion requires operation on kerosene-based jet fuels. These low vapor pressure fuels remain in liquid form at typical pulsed detonation inlet conditions and residence times, and the subsequent presence of fuel droplets significantly hinders performance. A fuel flash vaporization system FVS was designed and built to reduce evaporation time and provide gaseous fuel to the PDE. Four fuels that vary in volatility and octane number were tested n-heptane, iso-octane, aviation gasoline, and JP-8. Results showed the FVS quickly provides a detonable mixture for all of the fuels tested without cooking the fuel lines. A significant result was the detonation of flash vaporized JP-8 in air without a pre-detonator.

Descriptors:

• *PULSES
• *HYDROCARBONS
• *JET ENGINE FUELS
• *VAPORIZATION
• *DETONATIONS
• AIR BREATHING ENGINES
• KEROSENE
• INLETS
• VAPOR PRESSURE
• PROPULSION SYSTEMS

Subject Categories:

• Air Breathing Engines (Unconventional)
• Fuels

Distribution Statement:

APPROVED FOR PUBLIC RELEASE