Search Results for “Ivanitsky G. М.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com Space technology. Missile armaments Tue, 02 Apr 2024 08:09:56 +0000 en-GB hourly 1 https://journal.yuzhnoye.com/wp-content/uploads/2020/11/logo_1.svg Search Results for “Ivanitsky G. М.” – Collected book of scientific-technical articles https://journal.yuzhnoye.com 32 32 2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop https://journal.yuzhnoye.com/content_2018_1-en/annot_2_1_2018-en/ Mon, 04 Sep 2023 12:45:06 +0000 https://journal.yuzhnoye.com/?page_id=30403
, Ivanitsky G. O., Ivanitsky G. O., Ivanitsky G. O., Ivanitsky G. Missile armaments Том: 2018 Випуск: 2018 (1) Рік: 2018 Сторінки: 6—12.doi: https://doi.org/10.33136/stma2018.01.006 . O., Ivanitsky G. Missile armaments Том: 2018 Випуск: 2018 (1) Рік: 2018 Сторінки: 6—12.doi: https://doi.org/10.33136/stma2018.01.006 . O., Ivanitsky G. Missile armaments Том: 2018 Випуск: 2018 (1) Рік: 2018 Сторінки: 6—12.doi: https://doi.org/10.33136/stma2018.01.006 . O., Ivanitsky G. Missile armaments Том: 2018 Випуск: 2018 (1) Рік: 2018 Сторінки: 6—12.doi: https://doi.org/10.33136/stma2018.01.006 .
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2. Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2018 (1); 6-12

DOI: https://doi.org/10.33136/stma2018.01.006

Language: Russian

Annotation: An alternative method of kerosene dehydration is proposed, which is based on application of cyclic technology of supersaturation decrease using dry nitrogen. A comparison of nitrogen and time specific consumption in dehydration operations is done and recommendations are given for their use in the cosmodromes’ launch complexes fuel storage and preparation facilities.

Key words:

Bibliography:

1. Zrelov V. N., Seryogin E. P. Liquid Rocket Propellants. М., 1975. 320 p.
2. Energy-Intensive Fuels for Aircraft and Rocket Engines / Under the editorship of L. S. Yanovsky. М., 2009. 400 p.
3. Soyuz-2. URL: https://ru.wikipedia.org/wiki/Soyuz-2_(launch vehicle family).
4. Angara. URL: https://ru.wikipedia.org/wiki/Angara_(launch vehicle).
5. Zenit-2. URL: https://ru.wikipedia.org/wiki/Zenit-2_(launch vehicle).
6. Leshchiner L. B., Ul’yanov I. E. Designing of Aircraft Fuel Systems. М., 1975. 344 p.
7. Zenit Space Launch System from the Eyes of its Developers / Under the editorship of e.d. professor V. N. Solov’yov, e.d. professor G. P. Biryukov, N. S. Kozhukhov, N. I. Kursenkova. М., 2003. 213 p.
8. Space Rocketry Ground Infrastructure Technological Facilities: Engineering Manual. Book 1. М., 2005. 416 p.
9. Investigation of Prospective Propellant Preparation Technologies: Scientific-Technical Report 21.18258.173ОТ / Yuzhnoye SDO. 2016. 115 p.
10. Shleifer A. A., Litvinov A. N. Prospective Technologies to Prepare Propellants with Improved Performance Properties. Ul’yanovsk, 1989. 215 p.
11. Englin B. A. Use of Liquid Propellants at Low Temperatures. 3-rd edition revised and enlarged. М., 1980. 207 p.
12. Volkov A. I., Zharsky I. M. Big Chemical Guide. Minsk, 2005. 608 p.
13. Calculated Evaluation and Experimental Check of RPC Degassing and Saturation by Helium for Filling Cyclone-4 LV: Technical Note Cyclone-4. 22.6849.123 СТ / Yuzhnoye SDO. 2005. 29 p.

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2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
2.1.2018 Dehydration of Hydrocarbon Fuels by Method of Over-Saturation Drop
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4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics https://journal.yuzhnoye.com/content_2017_2/annot_4_2_2017-en/ Tue, 08 Aug 2023 12:33:25 +0000 https://journal.yuzhnoye.com/?page_id=29746
Ivanitsky, S. (2017) "Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics" Космическая техника. "Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics" Космическая техника. quot;Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics", Космическая техника.
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4. Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 19-24

Language: Russian

Annotation: The main directions of upgrading the pneumohydraulic systems are considered. Some methods of increasing their operability and reliability are analyzed.

Key words:

Bibliography:
1. Belyayev N. M. Rocket Propellant Tanks Pressurization Systems. М., 1976.
2. Kozlov A. A., Novikov V. N., Solov’yov E. V. Liquid Rocket Propulsion Systems Feeding and Control Systems. М., 1988.
3. Patent 51806, Ukraine, MPK В64Д 37/00. Rocket Propellant Tank Pressurization Method / B. A. Shevchenko, Y. A. Mitikov, А. I. Logvinenko (Ukraine). Applicant and patent holder Yuzhnoye SDO. No. 2000031474; Claimed 15.03.2002; Published 16.12.2002, Bulletin No. 12.
4. Patent 72330, Ukraine, MPK F02K 9/44, F02K 11/00. Method of Propellant Residues Utilization in Liquid Rocket Propulsion System / G. M. Ivanitsky, S. N. Kubanov, А. I. Logvinenko, G. I. Yushin (Ukraine); Applicant and patent holder Yuzhnoye SDO. No. 200210267; Claimed 16.12.2002; Published 15.02.2005, Bulletin No. 2.
5. Logvinenko A. I. Evolution Tendencies of LV Propellant Tanks Pressurization Systems. Paper presentation at IAA Congress (Fukuoka, Japan, October 2005). Dnepropetrovsk, 2005.
6. Mashchenko A. N., Logvinenko A. I. Passivation of LV Upper Stages Propellant Systems: Effective Means of Space Debris Control. Paper presentation at IAA Congress (Hyderabad, India, October 2007). Dnepropetrovsk, 2007.
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4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
4.2.2017 Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics
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