Effects of Nano-Aluminium on The Combustion of A PolyNIMMO-Based Propellant

被引:0
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作者
Clive Woodley
Peter Henning
机构
[1] QinetiQ,MODFortHalstead,Sevenoaks,KentTNBP,UnitedKingdom
关键词
physical chemistry; closed vessel; burn rate; nano-aluminium; wear and erosion; poly(nitratomethyl methyl oxetane) base propellant;
D O I
10.14077/j.issn.1007-7812.2014.06.002
中图分类号
V51 [航天用燃料(推进剂)及润滑剂];
学科分类号
080502 ;
摘要
Propellants containing micro-aluminium particles have been shown to produce faster burn rates than conventional gun propellants.However,they are also more abrasive than conventional propellants.Nano-material propellants have been reported to give similar benefits to micron-material propellants but without the disadvantage of increased abrasion.Tests were conducted to compare the burn rates,ignitability and wear rates of a propellant loaded with 0% aluminium,15% micro-aluminium and 15%nano-aluminium.Closed vessel tests showed a burn rate increase of 39% in the range 30-250 MPa,and 70% at low pressure(50-100MPa)for the nano-aluminium propellant compared with the baseline propellant.The micro-aluminium propellant showed only a 10%increase in the burn rate compared with the standard propellant.The ignition delay for the nano-aluminium propellant was slightly shorter than that of the baseline propellant.Substantially increased wear rates were measured for the micro-aluminium propellant.The nano-aluminium propellant showed reduced wear rates compared with the micro-aluminium propellant but these were still substantially greater than those for the baseline propellant.
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页码:7 / 11
页数:5
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