Zobrazeno 1 - 10
of 105
pro vyhledávání: '"air-launch"'
Autor:
A. A. Khramov
Publikováno v:
Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 23, Iss 1, Pp 80-92 (2024)
The problems of optimizing the trajectory motion of the first stage of an aerospace system according to the criterion of the maximum of the final mass are considered. The control is the angle of attack and thrust of the engines. Control optimization
Externí odkaz:
https://doaj.org/article/45eedff927484a6e918d3208570cb443
Autor:
Olejnik, Aleksander, Zalewski, Piotr, Kiszkowiak, Łukasz, Rogólski, Robert, Dziubiński, Adam, Frant, Michał, Majcher, Maciej, Omen, Łukasz
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2022, Vol. 95, Issue 4, pp. 629-636.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2022-0041
Publikováno v:
Przegląd Nauk o Obronności / Defence Science Review. (13):101-114
Externí odkaz:
https://www.ceeol.com/search/article-detail?id=1107462
Publikováno v:
Defence Science Review, Iss 13, Pp 101-114 (2022)
Objectives The study was to analyze the concept of Responsive Space Systems alternative launch and set of the nanomicro satellites into Low Earth Orbit. The analysis focused on aircraft-rocket space systems, where platform for launching a rocket wit
Externí odkaz:
https://doaj.org/article/d3ed1992eded45a292390198fc9687e4
Autor:
Aleksander Olejnik, Piotr Zalewski
Publikováno v:
Biuletyn Wojskowej Akademii Technicznej, Vol 69, Iss 3, Pp 89-103 (2020)
The work is an announcement on the current state of the research project implementation. The study presents the results of an analysis of the project’s research area. On this basis, the two-stage micro-satellite launch system was selected. The syst
Externí odkaz:
https://doaj.org/article/c4963b1c7a5c4746b5a6e2fe39e3e35d
Autor:
Aleksandrs Urbahs, Sergey Kravchenko, Margarita Urbaha, Kristine Carjova, Natalja Panova, Rafal Chatys
Publikováno v:
Aviation, Vol 25, Iss 2, Pp 73-78 (2021)
The paper presents the air-launch system enabling the delivery of small satellites into low Earth orbit. One of the most important advantages of the concept is its cost. Generally, the paper proves that launching a carrier from an aerial platform (a
Externí odkaz:
https://doaj.org/article/01e6d9dc3a8e40388f077d89188034ea
Publikováno v:
Hangkong gongcheng jinzhan, Vol 11, Iss 2, Pp 184-190 (2020)
At present, the research on air launch technology at home and abroad focuses on the numerical simulation and aerodynamic characteristics in the process of rocket separation, while the research on the impact of air launch on the payload of launch vehi
Externí odkaz:
https://doaj.org/article/e95a3781f2ed480e937bbbd7b6e4a730
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 12, Iss 6, Pp 1885-1903 (2019)
This paper explores the effect of design variables on the objective functions of clipped delta wing with a modified double-wedge airfoil section based on parametric analysis and CFD-based optimization using response surface method. This type of wing
Externí odkaz:
https://doaj.org/article/32a2aa29eec8465a9fc547ce61704410
Akademický článek
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Autor:
Piotr Zalewski, Aleksander Olejnik
Publikováno v:
Biuletyn Wojskowej Akademii Technicznej, Vol 69, Iss 3, Pp 89-103 (2020)
The work is an announcement on the current state of the research project implementation. The study presents the results of an analysis of the project’s research area. On this basis, the two-stage micro-satellite launch system was selected. The syst
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::24c107100664c002fc6469bc0bc8fd63
http://biuletynwat.pl/gicid/pdf/01.3001.0014.8874
http://biuletynwat.pl/gicid/pdf/01.3001.0014.8874