Development of a Solid, Low-Smoke Rocket Propellant – Smoke Generation Intensity Tests Using a Laser and Photodiode Setup

The work completed and discussed in this paper was to determine the level of smoke generation intensity in a selection of solid rocket propellants developed to minimise the level of generated smoke. This is an important issue for the application of the developed low-smoke propellant in, for example,...

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Những tác giả chính:	Przemysław WOŹNIAK (przemyslaw.wozniak.dokt@pw.edu.pl), Jan KINDRACKI (Jan.Kindracki@pw.edu.pl), Krzysztof WACKO (krzysztof.wacko@pw.edu.pl), Tomasz GOŁOFIT (tomgol@ch.pw.edu.pl), Michał CHMIELAREK (michal.chmielarek@pw.edu.pl), Katarzyna CIEŚLAK (kcieslak@ch.pw.edu.pl), Sylwia KOZŁOWSKA (sylwia.kozlowska3.dokt@pw.edu.pl), Paweł MAKSIMOWSKI (pmaksimowski@ch.pw.edu.pl), Łukasz MĘŻYK (lukasz.mezyk@pw.edu.pl), Maciej KOŁODZIEJ (maciej.kolodziej.dokt@pw.edu.pl), Dominik ZDYBAŁ (dominik.zdybal.dokt@pw.edu.pl)
Định dạng:	Artigo
Ngôn ngữ:	Inglês
Được phát hành:	Military University of Technology, Warsaw 2023-09-01
Loạt:	Problemy Mechatroniki
Những chủ đề:	rocket motor solid propellant combustion smoke generation laser
Truy cập trực tuyến:	http://promechjournal.pl/gicid/01.3001.0053.8819
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