Search Results for “Brezgin М. S.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 07:42:23 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Brezgin М. S.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants https://journal.yuzhnoye.com/content_2017_2/annot_7_2_2017-en/ Tue, 08 Aug 2023 12:43:00 +0000 https://journal.yuzhnoye.com/?page_id=29758
, Brezgin М. Y., Brezgin М. (2017) "Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants" Космическая техника. "Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants" Космическая техника. Y., Brezgin М. quot;Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants", Космическая техника. Y., Brezgin М. Missile armaments Том: 2017 Випуск: 2017 (2) Рік: 2017 Сторінки: 35—40.doi: . Y., Brezgin М. Missile armaments Том: 2017 Випуск: 2017 (2) Рік: 2017 Сторінки: 35—40.doi: . Y., Brezgin М. Missile armaments Том: 2017 Випуск: 2017 (2) Рік: 2017 Сторінки: 35—40.doi: . Y., Brezgin М. Missile armaments Том: 2017 Випуск: 2017 (2) Рік: 2017 Сторінки: 35—40.doi: .
]]>

7. Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants

Authors:

Mikhalchishin R. V., Kuda S. А., Golovin D. Y., Brezgin М. S.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 35-40

Language: Russian

Annotation: The paper presents the results of comparative investigation into characteristics of methane, kerosene and hydrogen in pair with oxygen. The peculiarities of each of these components are shown. The optimal parameters are considered of pneumohydraulic supply system, including the designs of tanks, pressurization system and engine supply lines cooling system.

Key words:

Bibliography:
1. Tamura H., Ono F., Kumakawa A. LOX/Methane Staged Combustion Rocket Investigation. AIAA 87-1856.
2. Crocker A., Perry S. System, Sensitivity Studies of a LOX/Methane Expander Cycle Upper Stage Engine. AIAA 98-3674.
3. Kyoung-Ho Kim, Dae-Sung Ju. Development of “Chase-10” liquid rocket engine having 10tf thrust using LOX & LNG (Methane). AIAA-2006-4907. 2014.
4. Evaluation of Parameters of Liquid Oxygen Circulation in Cryogenic LRPS Colling System: Technical Note 22.8234.123 ST / Yuzhnoye SDO. 2014.
5. Belyayev N. M. Pneumohydraulic Systems. Calculation and Designing. М., 1988. 42 p.
6. Pavlyuk Y. S. Ballistic Designing of Rockets: Tutorial for universities. Chelyabinsk, 1996. 92 p.

Full text (PDF) || Content 2017 (2)

Downloads: 36
Abstract views: 
541
Dynamics of article downloads
Dynamics of abstract views
Downloads geography
CountryCityDownloads
USA Boardman; Matawan; Baltimore; Phoenix; Monroe; Ashburn; Seattle; Seattle; Ashburn; Ashburn; Boardman; Tappahannock; San Mateo; San Mateo; San Mateo; Des Moines; Boardman; Boardman; Ashburn; Boardman20
Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore; Singapore8
Ukraine Dnipro; Dnipro2
Unknown Melbourne1
Finland Helsinki1
Canada Monreale1
Germany Falkenstein1
Romania Voluntari1
Netherlands Amsterdam1
Downloads, views for all articles
Articles, downloads, views by all authors
Articles for all companies
Geography of downloads articles
7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants
7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants
7.2.2017 Features of Pneumatic Hydraulic Feeding System with the Use of Oxygen-Methane Cryogenic Propellants
]]>