Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Marcin Cegła"'
Publikováno v:
Problemy Mechatroniki, Vol 10, Iss 2, Pp 43-54 (2019)
The paper presents results of thermal decomposition analysis of selected solid rocket propellants. Homogeneous propellant PAC and heterogeneous propellant H2 were subjected to simultaneous thermal analysis with the use of NETZSCH STA 2500 Regulus dev
Externí odkaz:
https://doaj.org/article/a4b77e0179c742ccae4720ff745add44
Publikováno v:
Biuletyn Wojskowej Akademii Technicznej, Vol 65, Iss 1, Pp 47-56 (2016)
The article presents dynamic mechanical analysis (DMA) for solid rocket propellants testing. Principles of operation and measured values are briefly described. The authors refer to the previous research of PTFE material and literature data providing
Externí odkaz:
https://doaj.org/article/5c1dd0b60c5f4e9b959086a682d3a763
Autor:
Marcin CEGŁA, Janusz ZMYWACZYK, Piotr KONIORCZYK, Maciej MISZCZAK, Jacek BORKOWSKI, Bogdan FLORCZAK
Publikováno v:
Problemy Mechatroniki, Vol 6, Iss 1, Pp 11-18 (2015)
The paper presents results of Dynamic Mechanical Analysis (DMA) of double-base (DB) solid rocket propellant with special attention paid to determining the glass transition temperature. The presented experiments were carried out with the use of Netzch
Externí odkaz:
https://doaj.org/article/c1f435f197434e1f9c9963972e74197d
Autor:
Pawel Zochowski, Marcin Cegła, Krzysztof Szczurowski, Jędrzej Mączak, Marcin Bajkowski, Ewa Bednarczyk, Roman Grygoruk, Mariusz Magier, Dariusz Pyka, Mirosław Bocian, Krzysztof Jamroziak, Roman Gieleta, Piotr Prasuła
Publikováno v:
Continuum Mechanics and Thermodynamics.
The main aim of the work was the experimental and numerical analysis of the energy absorption/dissipation capabilities and failure mechanisms of novel hyper-elastic target material intended for ballistic applications including layers of composite arm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1031252d96f73c410625d4e4a3cc4d2a
https://doi.org/10.1007/s00161-023-01210-2
https://doi.org/10.1007/s00161-023-01210-2
Publikováno v:
International Journal for Numerical Methods in Biomedical Engineering. 39
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::17c400a2b7a329077fa9cf4b10513d0f
https://doi.org/10.1002/cnm.3687
https://doi.org/10.1002/cnm.3687
Publikováno v:
Problemy Mechatroniki, Vol 10, Iss 2, Pp 43-54 (2019)
The paper presents results of thermal decomposition analysis of selected solid rocket propellants. Homogeneous propellant PAC and heterogeneous propellant H2 were subjected to simultaneous thermal analysis with the use of NETZSCH STA 2500 Regulus dev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d2086ff9a6401d6101ebd58e42adbb1a
https://doi.org/10.5604/01.3001.0013.2115
https://doi.org/10.5604/01.3001.0013.2115
Publikováno v:
PROBLEMY TECHNIKI UZBROJENIA. 147:105-121
The article presents results of thermo-mechanical analysis of heterogeneous solid rocket propellant H2, with special attention devoted to determining the glass transition temperature and softening temperature. Mechanical properties such as storage mo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::83ac443024ddd186e9a02bb6838837d9
https://doi.org/10.5604/01.3001.0012.8315
https://doi.org/10.5604/01.3001.0012.8315
Autor:
Marcin Cegła
Publikováno v:
PROBLEMY TECHNIKI UZBROJENIA. 147:63-74
The paper presents some questions of designing and testing for modern ballistic protecting screens and applied materials especially such as ceramics. Continuous development of present ballistic composite materials enforces the optimisation of existin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d1e0a6679a2143c3e702ef31387fcc1
https://doi.org/10.5604/01.3001.0012.8312
https://doi.org/10.5604/01.3001.0012.8312
Publikováno v:
AIP Conference Proceedings.
The paper presents results of experimental research of three types of homogeneous double-base solid rocket propellants with special attention given to the determination of glass transition temperature and calculating activation energy of the transiti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::901e61d48b2258ddf215743c06160088
https://doi.org/10.1063/1.5120138
https://doi.org/10.1063/1.5120138
Publikováno v:
AIP Conference Proceedings.
The paper presents results of experimental research of selected solid rocket propellants with the use of modern thermal analysis techniques. Differential Scanning Calorimetry (DSC) was used to determine specific heat values in the temperature range f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2747ee8125a5c13ac2072a1fa9d86121
https://doi.org/10.1063/1.5120137
https://doi.org/10.1063/1.5120137