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4. Increase of LV Payload Capability through Enhancement of Propulsion System Pneudraulic System Characteristics

e-ISSN: 2617-5533

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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