A novel 6 dof thrust vector control test stand
Апстракт
This study proposes an innovative test stand design to accurately measure rocket motor thrust vector during its operation. Test stand design is clearly presented as well as procedure and mathematical model for its calibration. A method of processing data obtained from the experiments and the results of the jet tab system for thrust vector control are presented in detail. Experiments have shown that the test stand is highly functional and the results obtained have excellent repeatability and matching with the results of the other authors who have used different construction test stands for measurement of the same or a similar mechanism for thrust vector control.
Кључне речи:
thrust vector control / test stand / rocket motor / jet tabИзвор:
Tehnički vjesnik, 2015, 22, 5, 1247-1254Издавач:
- Univ Osijek, Tech Fac, Slavonski Brod
Финансирање / пројекти:
- Космички транспортни системи ниске цене (RS-MESTD-Technological Development (TD or TR)-35044)
DOI: 10.17559/TV-20140621064603
ISSN: 1330-3651
WoS: 000363986400022
Scopus: 2-s2.0-84946020459
Колекције
Институција/група
Mašinski fakultetTY - JOUR AU - Miloš, Predrag AU - Davidović, Nikola AU - Jojić, Branislav AU - Miloš, Marko AU - Todić, Ivana PY - 2015 UR - https://machinery.mas.bg.ac.rs/handle/123456789/2228 AB - This study proposes an innovative test stand design to accurately measure rocket motor thrust vector during its operation. Test stand design is clearly presented as well as procedure and mathematical model for its calibration. A method of processing data obtained from the experiments and the results of the jet tab system for thrust vector control are presented in detail. Experiments have shown that the test stand is highly functional and the results obtained have excellent repeatability and matching with the results of the other authors who have used different construction test stands for measurement of the same or a similar mechanism for thrust vector control. PB - Univ Osijek, Tech Fac, Slavonski Brod T2 - Tehnički vjesnik T1 - A novel 6 dof thrust vector control test stand EP - 1254 IS - 5 SP - 1247 VL - 22 DO - 10.17559/TV-20140621064603 ER -
@article{ author = "Miloš, Predrag and Davidović, Nikola and Jojić, Branislav and Miloš, Marko and Todić, Ivana", year = "2015", abstract = "This study proposes an innovative test stand design to accurately measure rocket motor thrust vector during its operation. Test stand design is clearly presented as well as procedure and mathematical model for its calibration. A method of processing data obtained from the experiments and the results of the jet tab system for thrust vector control are presented in detail. Experiments have shown that the test stand is highly functional and the results obtained have excellent repeatability and matching with the results of the other authors who have used different construction test stands for measurement of the same or a similar mechanism for thrust vector control.", publisher = "Univ Osijek, Tech Fac, Slavonski Brod", journal = "Tehnički vjesnik", title = "A novel 6 dof thrust vector control test stand", pages = "1254-1247", number = "5", volume = "22", doi = "10.17559/TV-20140621064603" }
Miloš, P., Davidović, N., Jojić, B., Miloš, M.,& Todić, I.. (2015). A novel 6 dof thrust vector control test stand. in Tehnički vjesnik Univ Osijek, Tech Fac, Slavonski Brod., 22(5), 1247-1254. https://doi.org/10.17559/TV-20140621064603
Miloš P, Davidović N, Jojić B, Miloš M, Todić I. A novel 6 dof thrust vector control test stand. in Tehnički vjesnik. 2015;22(5):1247-1254. doi:10.17559/TV-20140621064603 .
Miloš, Predrag, Davidović, Nikola, Jojić, Branislav, Miloš, Marko, Todić, Ivana, "A novel 6 dof thrust vector control test stand" in Tehnički vjesnik, 22, no. 5 (2015):1247-1254, https://doi.org/10.17559/TV-20140621064603 . .