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, Yakimets S. 2017 (2); 60-64 Language: Russian Annotation: The calculation procedure is proposed, the analysis is made and the ranges of optimal probability values of no-failure operation of pneumohydraulic propellant supply system and its elements are determined based on general requirements to integrated launch vehicle. Ensuring Reliability of Prospective Injection Means. Dnepropetrovsk, 2000. System Approach to Development of Modular Launch Vehicle Family / A. P., Yakimets S. P., Yakimets S. Missile armaments, vol. P., Yakimets S. P., Yakimets S. P., Yakimets S. P., Yakimets S. More Citation Formats Harvard Chicago IEEE AIP ДСТУ 8302:2015 ДСТУ ГОСТ 7.1:2006 (ВАК) ISO 690:2010 BibTeX на сайт ДП «КБ «Південне»
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12. Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability

Authors:

Nazarenko O. P., Yakimets S. V.

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 60-64

Language: Russian

Annotation: The calculation procedure is proposed, the analysis is made and the ranges of optimal probability values of no-failure operation of pneumohydraulic propellant supply system and its elements are determined based on general requirements to integrated launch vehicle.

Key words:

Bibliography:
1. Berlow R., Proshan F. Statistic Reliability Theory and Dependability Tests / Translation from English. М., 1984. 328 p.
2. Lloyd D., Lipov M. Reliability. Organization of Investigation, Methods, Mathematical Apparatus / Translation from English; Under the editorship of Buslenko N. P. М.,1964. 686 p.
3. Ensuring Reliability of Prospective Injection Means. URL: http://www. sciential.ru/technology/kosmos/199.html.
4. Yuzhnoye SDO Rockets and Spacecraft / Under general editorship of S. N. Konyukhov. Dnepropetrovsk, 2000. 236 p.
5. Degtyarev A. V. et al. System Approach to Development of Modular Launch Vehicle Family / A. V. Degtyarev, А. E. Kahanov, N. G. Litvin, V. A. Shulga. DNU News (Series RKT; Issue 15). Vol. 1. 2012.
6. Reliability Analysis of Taurus-II LV Stage One Core Structure Pneumohydraulic Propellants Supply System: Technical Report / Taurus-II. 21.18231.123 ОТ. Yuzhnoye SDO, 2016. 35 p.

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12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability
12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability
12.2.2017 Determination Procedure for Pneudraulic System and Its Components No-Failure Operation Probability
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