Search Results for “Kabakova Zh. V.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 08:02:47 +0000 en-GB hourly 1 https://wordpress.org/?v=6.2.2 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Kabakova Zh. V.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 25.2.2017 Vacuum Conditions Simulation Criteria https://journal.yuzhnoye.com/content_2017_2/annot_25_2_2017-en/ Wed, 09 Aug 2023 12:46:44 +0000 https://journal.yuzhnoye.com/?page_id=29958
Organization: Yangel Yuzhnoye State Design Office, Dnipro, Ukraine Page: Kosm. Kuda, Zh. Kabakova, A. Porubaimekh (Ukraine); Applicant and patent holder Yuzhnoye SDO.
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25. Vacuum Conditions Simulation Criteria

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 141-145

Language: Russian

Annotation: The paper shows the peculiarities of modeling the vacuum conditions to simulate space environment when conducting various test types. Based on generalized experience, the practical criteria are recommended with consideration for accompanying physical phenomina.

Key words:

Bibliography:
1. Rozanov L. N. Vacuum Engineering. М., 1990. 320 p.
2. Polukhin D. A., Oreshchenko V. M., Morozov V. A. Testing of Pneumohydraulic Subsystems of Propulsion Systems of LV and SC with LRE. М., 1987.
3. Deshman S. Scientific Basis of Vacuum Engineering. М., 1970.
4. Borisenko A. I. Gas Dynamics of Engines. М., 1962. 793 p.
5. Avduyevsky V. S. Fundamentals of Heat Transfer in Aerospace Engineering. М., 1975. 623 p.
6. Burdakov V. P., Danilov Y. I. External Resources and Cosmonautics. М., 1976. 551 p.
7. Kuda S. A. et al. Investigation of Freezing Conditions of Liquid Nitrogen in Manifolds at Flowing into Vacuum / S. A. Kuda, Zh. V. Kabakova, A. I. Logvinenko, V. I. Porubaimekh. Space Technology. Missile Armaments: Collection of scientific-technical articles. 2007. Issue 2. P. 58 – 67.
8. Patent 110307 Ukraine, MPK F25J 1/00. Method of Producing Overcooled Cryogenic Liquid / D. I. Gudymenko, S. A. Kuda, А. I. Logvinenko, V. I. Porubaimekh (Ukraine); Applicant and patent holder Yuzhnoye SDO. No 201601457; Claimed 18.02.2016; Published 10.10.2016, Bulletin No. 19.
Downloads: 19
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341
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25.2.2017 Vacuum Conditions Simulation Criteria
25.2.2017 Vacuum Conditions Simulation Criteria
25.2.2017 Vacuum Conditions Simulation Criteria
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19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation https://journal.yuzhnoye.com/content_2017_2/annot_19_2_2017-en/ Wed, 09 Aug 2023 12:23:07 +0000 https://journal.yuzhnoye.com/?page_id=29862
Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation Authors: Kabakova Zh. Content 2017 (2) Downloads: 19 Abstract views: 218 Dynamics of article downloads Dynamics of abstract views Downloads geography Country City Downloads USA Boardman; Baltimore; Dublin; Monroe; Ashburn; Ashburn; Seattle; San Mateo; Boardman; Ashburn; Boardman 11 Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore 6 Ukraine Dnipro; Dnipro 2 Downloads, views for all articles Articles, downloads, views by all authors Articles for all companies Geography of downloads articles Kabakova Zh. Kabakova Zh. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation Автори: Kabakova Zh. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation Автори: Kabakova Zh. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation Автори: Kabakova Zh.
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19. Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 107-111

Language: Russian

Annotation: The paper presents the generalized experience of designing and development testing of the pneumatic system for nose aerodynamic fairing halves jettisoning. The algorithm of its parameters calculation is given. The satisfactory convergence of the pneumatic system parameters calculation results with the experimental data from the ground and flight tests is shown.

Key words:

Bibliography:
1. Basis of Calculation of Gas Parameters in Pneumatic Systems Operation: Teacher Edition of Yuzhnoye SDO. 21.7217.123 ОТ. 1988.
2. Cyclone-4 SLS. Analysis of Experimental Data on PLF Doors Jettison Pneumatic System: Technical Report / Yuzhnoye SDO. Cyclone-4 21.17689.213 ОТ. 2014.
Downloads: 19
Abstract views: 
218
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USA Boardman; Baltimore; Dublin; Monroe; Ashburn; Ashburn; Seattle; San Mateo; Boardman; Ashburn; Boardman11
Singapore Singapore; Singapore; Singapore; Singapore; Singapore; Singapore6
Ukraine Dnipro; Dnipro2
19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation
19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation
19.2.2017 Experience in Development of Pneumatic System for Aerodynamic Payload Fairing Separation
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