المؤلفون: De Angelo, Bianca A.

الموضوعات: Liquid propellant rocket engines Cooling., Rockets (Aeronautics) Nozzles Cooling.

مصطلحات الفهرس: Aerodynamics and Fluid Mechanics, Aerospace Engineering, Propulsion and Power

URL: https://commons.erau.edu/edt/206Test

المؤلفون: Mohammed Amine DJEFFAL, Nabil BENAMARA, Abdelkader LAHCENE, Ali BENOUAR, Abdelkader BOULENOUAR, Mohammed MERZOUG

المصدر: INCAS Bulletin, Vol 16, Iss 1, Pp 33-44 (2024)

مصطلحات موضوعية: regenerative cooling, supercritical pressure methane, heat transfer deterioration, liquid propellant rocket engines, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://bulletin.incas.ro/files/djeffal_all__vol_16_iss_1.pdfTest; https://doaj.org/toc/2066-8201Test; https://doaj.org/toc/2247-4528Test

الوصول الحر: https://doaj.org/article/8a7e11e905544a42bdcb92c47acb539aTest

المؤلفون: A. D. Maksimov, S. A. Shustov

المصدر: Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, Vol 21, Iss 1, Pp 67-80 (2022)

مصطلحات موضوعية: low-thrust liquid-propellant rocket engines, thermogasdynamic calculation, propulsion unit, specific impulse, mach number, reynolds number, navier-stokes equations, specific impulse loss, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: https://journals.ssau.ru/vestnik/article/viewFile/10246/9015Test; https://doaj.org/toc/2542-0453Test; https://doaj.org/toc/2541-7533Test

الوصول الحر: https://doaj.org/article/00c6f162571b407988fd114fa89f5516Test

المؤلفون: Mitikov, Yurii, Shynkarenko, Olexiy

المصدر: Journal of Aerospace Technology and Management. January 2022 14

مصطلحات موضوعية: Dry mass reduction, Pressure reduction, Liquid propellant rocket engines, Helium, Pressure regulators, Propellant tanks

وصف الملف: text/html

الوصول الحر: http://old.scielo.br/scielo.php?script=sci_arttext&pid=S2175-91462022000100300Test

المؤلفون: Maurício Sá Gontijo

المصدر: Авіаційно-космічна техніка та технологія, Vol 0, Iss 4sup1 (2022)

مصطلحات موضوعية: vaporization models, liquid propellant rocket engines, characteristic length, injected droplet size, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

العلاقة: http://nti.khai.edu/ojs/index.php/aktt/article/view/1766Test; https://doaj.org/toc/1727-7337Test; https://doaj.org/toc/2663-2217Test

الوصول الحر: https://doaj.org/article/784df1871f2640bb82957e26dae0db01Test

المؤلفون: Aiswarya, N.¹, Suja Priyadharsini, S.¹ sujapriya_moni@yahoo.co.in, Moni, K. S.²

المصدر: Australian Journal of Mechanical Engineering. Oct2018, Vol. 16 Issue 3, p163-172. 10p.

مصطلحات موضوعية: *DEBUGGING, *LIQUID propellant rocket engines, *PROPULSION systems, *TIME-domain analysis, *FAST Fourier transforms

المؤلفون: Nguyen, Tuan M.¹ tuanmn2@uci.edu, Sirignano, William A.¹ sirignan@uci.edu

المصدر: Combustion & Flame. Sep2018, Vol. 195, p170-182. 13p.

مصطلحات موضوعية: *AXIAL flow, *LIQUID propellant rocket engines, *COMBUSTION chambers, *OXIDIZING agents, *MATHEMATICAL models of turbulence, *PROBABILITY density function

المؤلفون: Lee, Kyelim¹, Cha, Jihyoung¹, Ko, Sangho¹ sanghoko@kau.ac.kr, Park, Soon-Young², Jung, Eunhwan²

المصدر: Acta Astronautica. Sep2018, Vol. 150, p15-27. 13p.

مصطلحات موضوعية: *LIQUID propellant rocket engines, *FAULT indicators, *KALMAN filtering, *COMPUTER simulation, *BIOENERGETICS, *MATHEMATICAL models

المؤلفون: Radhakrishnan, Kanmaniraja¹, Son, Min², Lee, Keonwoong¹, Koo, Jaye^1,3 jykoo@kau.ac.kr

المصدر: Acta Astronautica. Sep2018, Vol. 150, p105-116. 12p.

مصطلحات موضوعية: *LIQUID propellant rocket engines, *PIVOT bearings, *JOULE-Thomson effect, *LAGRANGIAN mechanics, *INJECTORS

المؤلفون: Pelevin, F. V.¹ pelfv@rambler.ru, Avraamov, N. I.¹, Ir’yanov, N. Ya.¹, Orlin, S. A.¹, Lozovetskii, V. V.¹ lozovetsky@mail.ru, Ponomarev, A. V.¹ alexmgtu@gmail.com

المصدر: Journal of Engineering Physics & Thermophysics. May2018, Vol. 91 Issue 3, p601-610. 10p.

مصطلحات موضوعية: *LIQUID propellant rocket engines, *HEAT exchangers, *REGENERATIVE cooling, *PHYSICS experiments, *HEAT transfer