Source: http://knit.mao.kiev.ua/en/archive/2017/1/02
Timestamp: 2019-04-23 18:21:08+00:00

Document:
1. Belousov I. I., Golubyatnik V. V., Eliseev A. V., et al. The concept of creating a reusable propulsion oxygenmethane liquid rocket engine, which uses a turbopump unit with two spaced turbine on one shaft. Bull. Voronezh State Technical University, 10 (N 5), 00—00 (2014).
2. Belousov I. I., Fomin V. M., Golubyatnik V. V., et al. Proof of Concept reusable liquid rocket engine propellants on components liquefied natural gas and oxygen. Bull. Voronezh State Technical University, 9 (N 4), 42—46 (2013).
3. Dyadin Y. A., Gushchin A. L. Gas hydrates. Sorovsky Educational J., N 3, 55—60 (1998).
4. Egorov A. V. Biogeochemistry of methane in the sediments of the Baltic and Black Seas: kinetic model diagenesis. Oceanology, 40 (N 5), 600—606 (2000).
5. Efimochkin A. F., Golubyatnik V. V., Eliseev A. V. Settlement and analytical evaluation of options for concepts of cryogenic rocket engine with afterburning of the reducing gas. Bull. Voronezh State Technical University, 8 (N 7.1), 102—106 (2012).
6. Efimochkin A. F., Rachuk V. S., Shostak A. V. Liquid rocket engine for a reusable space-rocket system. NTG Aerospace engineering and technology, N 4, 26—36 (2010).
7. Efimochkin A. F., Chrysanthos S. P., Golubyatnikov V. V., et al. The development of liquid rocket engine propellants liquefied natural gas and oxygen for reusable space-rocket system. Vestnik of Samara University. Aerospace and Mechanical Engineering, N 3 (34), 253—259 (2012).
8. Efimochkin A. F., Chrysanthos S. P., Kafarena P. V., et al. Research of working process in rocket engine chamber working on fuel liquefied natural gas (LNG) — oxygen. NTG Aerospace engineering and technology, N 4, 21—25 (2010).
9. Ivanova I. K., Semenov M. E., Shilova Y. E., et al. Determination of temperature and pressure conditions for the formation of natural gas hydrates in emulsions of asphalt deposits. Fundamental res., N 2, 5089—5093 (2015).
10. Istomin V. A., Yakushev V. S. Gas hydrates under natural conditions, 236 p. (Nedra, Мoscow, 1992).
11. Levenko O. S. Universal LRE. Technical Proposal. Mechanics of aerospace systems: Monograph, 100 p. (Stylus, D., 2012).
12. Orehov K. N. Improved meteorological rockets in the application of hybrid engines. Kosm. nauka tehnol., 22 (2), 52—59 (2016).
13. Pat. 2166348 Russian Federation. The apparatus for producing gas hydrate / Melnikov V. P., Nesterov A. N., Feklistov V. V. Bulletin, N 13 (10.05.2001).
15. Prisyzhniy V. I., Levenko O. S., Pauk O. L. Aspects of the creation of the orbiter in the form of remote sensing satellite and the launch vehicle. Kosm. nauka tehnol., 20 (4), 3—13 (2014).
16. Sarner S. F. Propellant chemistry, (Мir, Moscow, 1969). 17. Semenov M. E., Shits E. Y. A study of the preparation of methane hydrates in static conditions. Oil and Gas Business, N 5, 457—465 (2012).
18. Solovyov V. A. Global assessment of the amount of gas in the submarine gas accumulation hydrates. Geology and geophys., 43 (7), 648—661 (2002).
19. Gaowei Hu and Yuguang Ye. Ultrasonic Waves on Gas Hydrates Experiments (Qingdao Institute of Marine Geology, China). Ultrasonic Waves. Ed. by Dr Santos, 282 p., Publ. online 07, March (2012), http://cdn.intechopen.com/pdfs/31680.pdf.

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