Rachid Amrousse Toshiyuki Katsumi Ahmed Bachar Rachid Brahmi Mohamed Bensitel Keiichi Hori
REACTION KINETICS MECHANISMS AND CATALYSIS 111(1) 71-88 2014年2月 [査読有り]
The influence of the catalyst support shapes on the performance of liquid monopropellant thrusters was investigated. In the present work, two supports: monolith honeycombs and alumina grains were tested and their relative performances were compare...
Hybrid rockets using Glycidyl Azide Polymer (GAP) as a solid fuel has been studied. Linear burning rate spectrum of GAP was spread with a dilution of polyethylene glycol (PEG), and basically, self combustible mixtures are used for the gas hybrid r...
International Journal of Energetic Materials and Chemical Propulsion 8(6) 555-570 2009年
A basic study to clarify the combustion mechanism of glycidyl azide polymer (GAP) has been conducted. Temperature during the strand burner and 60-mm diameter motor tests was measured. The strand tests were performed with 2.5-m diameter S-type ther...
Shogo Tomiyama Keiichi Hori Toshiyuki Katsumi Yutaka Wada Makihito Nishioka
International Journal of Energetic Materials and Chemical Propulsion 8(4) 267-280 2009年 [査読有り]
Currently, the market of airbag inflators as automobile safety devices is still expanding and the key technology in airbag inflation depends on the performance of a gas generant inside the inflator. The gas generant has been developed for modifyin...
SENSORS AND ACTUATORS A-PHYSICAL 144(2) 361-366 2008年6月
In this study, reactive B/Ti multilayer igniters were investigated for the noncontact ignition of a micro solid rocket array thruster in vacuum. When current is supplied to the B/Ti multilayer igniter, the chemical reaction: 2B + Ti -> TiB2 + 1320...
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