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NASA NTRS · 20060056182

Metallized Gelled Propellants Combustion Experiments in a Pulse Detonation Engine

Abstract

A series of combustion tests were performed with metallized gelled JP 8/aluminum fuels in a Pulse Detonation Engine (PDE). Nanoparticles of aluminum were used in the 60 to 100 nanometer diameter. Gellants were also of a nanoparticulate type composed of hydrocarbon alkoxide materials. Using simulated air (a nitrogen-oxygen mixture), the ignition potential of metallized gelled fuels with nanoparticle aluminum was investigated. Ignition of the JP 8/aluminum was possible with less than or equal to a 23-wt% oxygen loading in the simulated air. JP 8 fuel alone was unable to ignite with less than 30 percent oxygen loaded simulated air. The tests were single shot tests of the metallized gelled fuel to demonstrate the capability of the fuel to improve fuel detonability. The tests were conducted at ambient temperatures and with maximal detonation pressures of 1340 psia.

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BibTeXRIS

Palaszewski, Bryan, Jurns, John, Breisacher, Kevin, Kearns, Kim. 2006-10-01. Metallized Gelled Propellants Combustion Experiments in a Pulse Detonation Engine. https://ntrs.nasa.gov/citations/20060056182

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