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Metallized Gelled Propellants Combustion Experiments in a Pulse Detonation Engine
Author(s) -
Bryan Palaszewski,
John Jurns,
Kevin Breisacher,
Kimberly Kearns
Publication year - 2004
Publication title -
36th aiaa/asme/sae/asee joint propulsion conference and exhibit
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2004-4191
Subject(s) - propellant , detonation , combustion , materials science , pulse (music) , ignition system , aerospace engineering , nuclear engineering , automotive engineering , engineering , explosive material , electrical engineering , chemistry , organic chemistry , detector
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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