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Grzegorz Rarata
Researcher at Instytut Lotnictwa
Publications - 34
Citations - 461
Grzegorz Rarata is an academic researcher from Instytut Lotnictwa. The author has contributed to research in topics: Hydrogen peroxide & Propellant. The author has an hindex of 8, co-authored 33 publications receiving 343 citations. Previous affiliations of Grzegorz Rarata include Warsaw University of Technology.
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Influence of ignition position and obstacles on explosion development in methane–air mixture in closed vessels
TL;DR: In this paper, an experimental study of influence of the ignition position and obstacles on explosion development in premixed methane-air mixtures in an elongated explosion vessel was presented. But the authors did not consider the impact of obstacles on the course of pressure.
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Determination of explosion parameters of methane-air mixtures in the chamber of 40 dm3 at normal and elevated temperature
TL;DR: In this article, the experimental results of the measurements of the explosion pressure and rate of explosion pressure rise as a function of molar methane concentration in the mixture with air in the 40m3 explosion chamber are presented.
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Brief review on passive and active methods for explosion and detonation suppression in tubes and galleries
TL;DR: In this article, the authors summarized previous studies on explosions, detonations, and the deflagration-to-detonation transition (DDT), and then discussed potential passive/active or hybrid methods for suppressing explosions and detonation in tubes and galleries.
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Development of the ILR-33 “Amber” sounding rocket for microgravity experimentation
Blazej Marciniak,Adam Okninski,Bartosz Bartkowiak,Michal Pakosz,Kamil Sobczak,Wojciech Florczuk,Damian Kaniewski,Jan Matyszewski,Pawel Nowakowski,Dawid Cieslinski,Grzegorz Rarata,Pawel Surmacz,Dominik Kublik,Damian Rysak,Jaromir Smetek,Piotr Wolanski +15 more
TL;DR: The ILR-33 sounding rocket for microgravity experiments has been developed at the Institute of Aviation in Warsaw, Poland as discussed by the authors, which enables performing experiments in microgravity for almost 150 seconds with an apogee over 100 km.