TO THE QUESTION OF RESEARCH OF PROCESSES OF HEAT EXCHANGE AT PRE-START COOLING DOWN THE SERVICE TUBES PU UPPER BLOCK LV
https://doi.org/10.15518/isjaee.2015.21.020
Abstract
The paper presents the study of heat transfer processes during prelaunch decreasing expenditure highways propulsion units (PU) upper stage (US) launch vehicles (LV) and cryogenic systems of the test bench (TB). Based on the consideration of the equations of conservation of mass and energy as applied to gas-cushion tank and the volume of the tank is filled with cryogenic fluid, the methods of mathematical simulation of processes of cooling. According to the results of bench and flight tests control coefficients are specified closing dependences on heat transfer and friction in heat capacity of the elements. TB and PU. The results of calculation and experimental studies of the processes of cooling consumable hydrogen and oxygen arteries obtained at bench and flight tests of RB, can be used for verification of computer models calculate during cryogenic systems TB and PU.
About the Authors
A. G. GaleevRussian Federation
Doctor of Science (Engineering Science), Professor
V. P. Firsov
Russian Federation
Department of aviation and space thermal engineering, head of cryogenic systems SIC MAI, winner of the RF Government prize in science and technology
I. V. Antyukhov
Russian Federation
researcher at the Department of aviation space thermotechnics, MAI
A. V. Galeev
Russian Federation
graduate studentDepartment of “Management of operationof rocket and space systems”
References
1. Галеев А.Г., Денисов К.П., Ищенко В.И., Лисейкин В.А., Сайдов Г.Г., Черкашин А.Ю. Испытательные комплексы и экспериментальная отработка жидкостных ракетных двигателей / под ред. Н.Ф. Моисеева. М.: Машиностроение/Машиностроение-Полет, 2012.
2. Костюк В.В., Фирсов В.П. Теплообмен и гидродинамика в криогенных двигательных установках. М.: Наука, 2015.
3. Гордеев В.А., Партола И.С., Фирсов В.П., Иванов В.П. Оптимизация процесса отработки ПГСП ракет и разгонных блоков / Научно-технические разработки КБ «Салют», 2006-2008. М.: Машиностроение, 2010. С. 284-291.
4. Гордеев В.А., Фирсов В.П. Комплект математических моделей ПГСП криогенного разгонного блока / Научно-технические разработки ОКБ-23 – КБ «Салют». М.: Воздушный транспорт, 2006. С. 320-333.
5. http://www.flowvision.ru.
6. Пригожин В.И., Коваль А.И., Савич А.Р. Опыт применения водорода в ОАО КБХА при проведении испытаний жидкостных ракетных двигателей, их агрегатов и энергоустановок // Альтернативная энергетика и экология – ISJAEE. 2008. № 3. C. 87-94.
7. Техника низких температур. Под ред. Е.И. Микулина, И.В. Марфениной, А.М. Архарова. М.: «Энергия», 1975.
8. Fredrik Hellström. Numerical computations of the unsteady flow in a radial turbine. March 2008 Technical Reports from Royal Institute of Technology KTH Mechanics. SE-100 44 Stockholm, Sweeden.
Review
For citations:
Galeev A.G., Firsov V.P., Antyukhov I.V., Galeev A.V. TO THE QUESTION OF RESEARCH OF PROCESSES OF HEAT EXCHANGE AT PRE-START COOLING DOWN THE SERVICE TUBES PU UPPER BLOCK LV. Alternative Energy and Ecology (ISJAEE). 2015;(21):156-166. (In Russ.) https://doi.org/10.15518/isjaee.2015.21.020