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pro vyhledávání: '"Solid-fuel rocket"'
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Autor:
Toth, Balint
Publikováno v:
Сборник доклади от Годишна международна научна конференция на Факултет „Авиационен“ на Национален военен университет „Васил Левски“ – гр. Долна Митрополия, 19 - 20 април 2018 г. / Proceedings of the Annual International Scientific Conference of the Aviation Faculty of the National Military University "Vasil Levski" - Dolna Mitropolia, 19 - 20 April 2018. :133-140
Externí odkaz:
https://www.ceeol.com/search/chapter-detail?id=681183
Publikováno v:
Defence Technology. 18:1886-1894
Improving the thermal decomposition performance of hexanitrohexaazaisowurtzitane (CL-20) by appropriate methods is helpful to promote the combustion performance of CL-20-based solid propellants. In this study, we synthesized a sandwich structure of C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::10acf7d2413385ab7eefca67dfd964df
https://doi.org/10.1016/j.dt.2021.08.017
https://doi.org/10.1016/j.dt.2021.08.017
Publikováno v:
Defence Technology. 18:1875-1885
This study numerically simulated and investigated the flow field characteristics of a typical dual-pulse solid rocket motor with a soft pulse separation device through thermal insulation ablation under high-temperature dual-pulse erosion. The ablatio
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2c100f5fd77a81b3342948b595355779
https://doi.org/10.1016/j.dt.2021.08.004
https://doi.org/10.1016/j.dt.2021.08.004
Publikováno v:
Defence Technology. 18:1552-1562
To further explore the damage characteristics and impact response of the shaped charge to the solid rocket engine (SRE) in storage or transportation, protective armor was designed and the shelled charges model (SCM)/SRE with protective armor impactin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18a06bac982763be9430861de9e5fc97
https://doi.org/10.1016/j.dt.2021.08.016
https://doi.org/10.1016/j.dt.2021.08.016
Autor:
José Luis Arauz-Lara, Gerardo Saucedo-Zárate, Marco Saucedo-González, Emmanuel Vázquez-Martínez, José Refugio Martínez-Mendoza, Ángel de la Cruz-Mendoza, Hernán González-Aguilar, Azdrubal Lobo-Guerrero
Publikováno v:
Journal of Spacecraft and Rockets. 59:1029-1032
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::de4f19f4b71433598edc94851d432789
https://doi.org/10.2514/1.a34999
https://doi.org/10.2514/1.a34999
Autor:
Zhe-jun Wang, Hong-fu Qiang
Publikováno v:
Defence Technology. 18:618-625
With the purpose of investigating the effects of confining pressure and aging on the mechanical properties of Hydroxyl-terminated polybutadiene (HTPB) based composite solid propellant, tensile tests of thermal accelerated aged propellant samples unde
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::736764d1865e1cd608f7fd4bc80b70ec
https://doi.org/10.1016/j.dt.2021.06.014
https://doi.org/10.1016/j.dt.2021.06.014
Autor:
Adam Okninski
Publikováno v:
Chinese Journal of Aeronautics. 35:128-154
This paper presents the topic of using solid rocket propulsion for de-orbiting spacecraft, in order to fulfil space debris mitigation requirements. The benefits and disadvantages of using such means are discussed. A dedicated system can be implemente
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90e56df9022f41a8f5fb4603f8dd8911
https://doi.org/10.1016/j.cja.2021.07.038
https://doi.org/10.1016/j.cja.2021.07.038
Publikováno v:
Chinese Journal of Aeronautics. 35:214-234
For the solid rocket with depletion shutdown system, effective energy management is significant to meet terminal constraints by exhausting excess energy. Several traditional energy management algorithms cannot satisfy the altitude constraint and path
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7dd95508d62c499a013c7f3fe2c401b5
https://doi.org/10.1016/j.cja.2021.06.020
https://doi.org/10.1016/j.cja.2021.06.020
Autor:
P. A. Ramakrishna, Gaurav Marothiya
Publikováno v:
International Journal of Energetic Materials and Chemical Propulsion. 21:73-85
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3156990fcbf51168519d327781104b6d
https://doi.org/10.1615/intjenergeticmaterialschemprop.2021038593
https://doi.org/10.1615/intjenergeticmaterialschemprop.2021038593