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DEVELOPMENT STAGES OF THE CRYOGENIC LAUNCH AND BENCH COMPLEXES OF THE ROCKET AND SPACE TECHNOLOGY

Abstract

The paper briefly describes the creation of PJSC “Cryogenmash”, which appearance and development is inextricably linked with the origin of the cryogenic engineering industry in the USSR, as well as the development of cosmonautics and rocket engineering. The paper describes the tasks solved by leading specialists to create infrastructure for providing the cryogenic fuel components, bench systems for testing of engines and missile blocks, thermo-vacuum chambers, thermostating systems of compartments and the high-boiling fuel components. It was noted that the domestic basic cryogenic equipment surpassed the ones of foreign firms in many respects and solved the issue of effective and explosion-proof operation technology at all stages of the construction of launch and stand complexes. The organization of effective and safe cooling processes in the flow of liquid hydrogen and oxygen at refueling of rocket tanks, which were used in the BR “Ehergy” systems, is considered in detail. The advantages of this technology are shown in comparison with cooling in the storage tanks by evacuation of the vapor space. The cold of liquid hydrogen leaving the vacuum system was used in the liquid oxygen deep cooling system of the “Buran” spacecraft. The paper deals with the development of thermostating systems for providing temperature and humidity parameters in the rocket sections, under which the stable and trouble-free operation of devices and mechanisms is guaranteed, as well as the thermostating of high-boiling components of the fuel. The emphasis is placed on the development of systems based on air turboexpander units instead of the vapor compression machines. The authors attach the importance to the creation of a number of space simulators, including one of the largest in the world (with a volume of 10,000 m 3 ). The tasks that have been solved for the successful operation of the equipment are considered: the problems of strength and stability of the camera shell, ensuring tightness, selection of powerful means for safe evacuation and other important aspects of creating space simulators. It is noted that the experience of creating cryogenic equipment for launching complexes is fully used in the creation of new cosmodromes and, above all, the “Vostochny” cosmodrome.

About the Authors

A. M. Domashenko
PJSC Cryogenmash
Russian Federation
Ph.D. (engineering); Senior Researcher, Chief Specialist of the PJSC Cryogenmash; Associate Professor at Low Temperatures Department of the National Research University “Moscow Power Institute”; Corresponding Member of the International Academy of Refrigeration


E. Yu. Tarasova
PJSC Cryogenmash
Russian Federation
Director of Research and Design Institute Cryogenmash


References

1. Domashenko A.M. Domestic rocket-space science and technology development. Launch and bench complexes (Razvitie otechestvennoi raketnokosmicheskoi nauki i tekhniki. Startovye i stendovye kompleksy). In: Development history of domestic rocket-space engine installations (Istoriya razvitiya otechestvennykh raketno-kosmicheskikh dvigatel’nykh ustanovok) / Ed. M.A. Pervov. Moscow: Stolichnaya enciklopediya, 2017, vol. 4, pp. 287–306 (in Russ.).

2. 65 years of JSC Cryogenmash / Ed. Mazin A.N. Balashiha: JSC Cryogenmash Publ., 2014, 196 p. (in Russ.).

3. Belyakov V.P. Cryogenic engineering and technology (Kriogennaya tekhnika i tekhnologiya). Moscow: Energoizdat Publ., 1982, 272 p. (in Russ.).

4. Arkharov A.M., Marfenina I.V., Mikulin E.I. Cryogenic systems. Book 1. Basis of the theory and calculation (Kriogennye sistemy, vol 1: Osnovy teorii i rascheta). Moscow: Mashinostroenie Publ., 1996, 576 p. (in Russ.).

5. Filin N.V. Cryogenics in rocket space technology (Kriogenika v raketno-kosmicheskoy tekhnike). In: Reports theses of XX scientific readings on cosmonautics (Tezisy dokladov XX nauchnykh chtenii po kosmonavtike). Moscow: RAS, 1996. (in Russ.)

6. Filin N.V., Bulanov A.B. Liquid cryogenic systems (Jidkostnye kriogennye sistemy). Moscow: Mashinostroenie Publ., 1985, 245 p. (in Russ.).

7. Domashenko A.M., Kachura V.P., Filin N.V. Experimental study of the nonequilibrium of evaporation during cooling of liquid oxygen and nitrogen by evacuation of the vapor space (Eksperimental’noe issledovanie neravnovesnosti ispareniya pri okhlazhdenii zhidkikh kisloroda i azota vakuumirovaniem parovogo prostranstva). In: Proceedings of SPA “Cryogenmash”. Processes and technologies in cryogenic engineering (Trudy NPO “Kriogenmash”. Processy i tekhnologii v kriogennom mashinostroenii). Balashikha, 1975. (in Russ.)

8. Domashenko A.M., Kachura V.P., Jolus S.N. Engineering calculation method of cryogenic liquid cooling in the boiling and evaporation mode (Injenernaya metodika rascheta okhlajdeniya kriogennykh jidkostei v rejime kipeniya i ispareniya). Khimicheskoe i neftyanoe mashinostroenie, 1976;(9):19–21 (in Russ.).

9. Filin N.V. Transition process in cryogenic systems (Perekhodnye processy v kriogennykh sistemakh). In: Modern cryogenics questions (Voprosy sovremennoi kriogeniki). Moscow: Vneshtorgizdat Publ., 1975, 238– 249 (in Russ.).

10. Filin N.V. Hydraulic shock investigations in deadlock branch of cryogenic pipe line (Issledovaniya gidravlicheskikh udarov v tupikovykh otvodakh kriogennykh truboprovodov). Khimicheskoe i neftyanoe mashinostroenie, 1975;(9):13–15 (in Russ.).

11. Filin N.V., Kacnel’son G.G., Klebanov A.I. Features of the regions formed before the shut-off valve (Osobennosti polostey, obrazuyushikhsya pered zapornoy armaturoy). Injenerno-fizicheskii jurnal, 1979;36(1):110–114 (in Russ.)

12. Kachura V.P., Filin N.V., Klebanov A.I. Fill dynamics of unchilled out pipeline by liquid nitrogen (Dinamika zapolneniya nezaholozhenoi magistrali zhidkim azotom). In: Digest of scientific papers of SPA Cryogenmash (Sbornik nauchnykh trudov NPO “Kriogenmash”). Balashikha, 1976, p. 55–71 (in Russ.).

13. Solov'ev V.N. The space rocket complex “Zenit” eyes of his creators FSUE DEDAM. Moscow: Moscow aviation institute Publ., 2003, 213 p. (in Russ.).

14. Domashenko A.M. Fire and explosion safety provision of liquid hydrogen obtaining, storage and transportation (Obespechenie vzryvopojarobezopasnosti system polucheniya, khraneniya i transportirovaniya jidkogo vodoroda). Tekhnicheskie gasy, 2014;(3):59–66 (in Russ.). [

15. Domashenko A.M., Krasovickii Yu.V., Krishtal V.N. Creation of various cryogenic filling and bench complexes of the rocket and space technology (Sozdanie razlichnykh kriogennykh zapravochnykh i stendovykh kompleksov raketno-kosmicheskoy tekhniki). Tekhnicheskie gasy, 2014;(4):40–48 (in Russ.).

16. Domashenko A.M. Сreation and improvement of cryogenic filling and bench complexes of the rocket and space technology (Sozdanie i sovershenstvovanie kriogennykh zapravochnykh i stendovykh kompleksov raketno-kosmicheskoi tekhniki). Tekhnicheskie gasy, 2009;(1):27–33 (in Russ.).

17. Domashenko A.M. Critical technologies for the cryogenic ground infrastructure creation. Cryogenic fuels application in perspective aircrafts (Kriticheskie tekhnologii sozdaniya kriogennoi nazemnoi infrastruktury. Primenenie kriogennykh topliv v perspektivnykh letatel’nykh apparatakh). In: Digest of VI science technical conference reports of Zhukovskii MATU (Sbornik dokladov VI nauchno-tekhnicheskoi konferencii VATU im. Zhukovskogo). Voronezh, 2002.

18. Domashenko A.M., Barabanov V.N., Kozlov Yu.V. Thermostating systems of the universal launch booster rocket complex (Sistemy termostatirovaniya universal'nogo startovogo kompleksa raketonositelei). Tekhnicheskie gasy, 2014;(3):68–71 (in Russ.).

19. Bogomolov A.A. Thermostating systems (Sistemy termostatirovaniya). In: “Zenit” space rocket complex through the eyes of its creators (Kosmicheskii raketnyi kompleks “Zenit” glazami ego sozdatelei). Moscow: Moscow Aviation Institute Publ., 2003, 132– 137 (in Russ.).

20. Dubinskii M.G., Martynovkii V.S. The air turborefrigerating machines with additional cooling in regenerator (Vozdushnye turbokhollodil’nye mashiny s dopolnitel’nym okhlazhdeniem v regeneratore). Kholodil’naya tekhnika, 1964;(6):16–18 (in Russ.).

21. Belyakov V.P. Highly effective cryosorption pump of a new construction (Vysokoeffektivnyi kriosorbcionnyi nasos novoi konstrukcii). In: Modern cryogenics questions (Voprosy sovremennoi kriogeniki). Moscow: Vneshtorgizdat Publ., 1975, 341–359 (in Russ.).

22. Kupriyanov V.I. The cryosorption pump for pumping out of large chamber (Krisorbcionnyi nasos dlya vakuumirovaniya krupnykh kamer). In: Atomic science and technology questions. Physics and equipment of high vacuum (Voprosy atomnoi nauki i tekhniki. Fizika i tekhnika vysokogo vakuuma). Kharkov: KPTI AS USSR Publ., 1977;2(8):72–73 (in Russ.).

23. Makarov A.M. High-vacuum systems calculated models of large cryogenic pressure chamber (Raschetnye modeli vysokovakuumnykh sistem krupnykh kriogennykh barokamer). In: Main directions and problems of vacuum pumping equipment creation (Osnovnye napravleniya i problemy sozdaniya vakuumnogo otkachnogo oborudovaniya). Moscow: Mashinostroenie Publ., 1976, 78–79 (in Russ.).

24. Borc B.V. Continious vacuum adsorption pump (Vakuumnyi adsorbcionnyi nasos nepreryvnogo deistviya). In: Theses of All-union Scientific and Technical Cooperation reports on cryogenic means of obtaining high vacuum (Tezisy dokladov vsesoyuznogo NTS po kriogennym sredstvam polucheniya vysokogo vakuuma). Kharkiv: KPTI AS USSR Publ., 1977, 22–24 (in Russ.).

25. Breslavec K.G. Some ways of operating efficiency increase of cryosorption pump with cold cavity (Nekotorye sposoby povysheniya effektivnosti raboty kriosorbcionnykh nasosov s kholodnoi polost’uy). Problems of Atomic science and technique. Voprosy atomnoi nauki i tekhniki. Fizika i tekhnika vysokogo vakuuma, 1977;2(8):76–79 (in Russ.).

26. Volchkevich A.I. High vacuum adsorption pump (Vysokovakuumnye adsorbcionnye nasosy). Moscow: Mashinostroenie Publ., 1973, 214 p. (in Russ.).

27. Garvik E.L. Cryogenic pumping out and space imitation (Kriogennaya otkachka i imitaciya kosmosa). In: New ways of cryogenic technique (Novye napravleniya kriogennoi tekhniki) / Ed. M.P.Malkov. Moscow: Mir Publ., 1966, 176–197 (in Russ.).

28. Gorbachev S.P. Low temperature fields calculation in cryogenic heat-absorbing screens (Raschet nizkotemperaturnykh polei v teplopogloshayushikh kriogennykh ekranakh). In: Proceedings of SPA Cryogenmash (Trudy NPO “Kriogenmash”). Balashikha, 1973;(15):73–85 (in Russ.).

29. Gerliga V.A. Stability of cryogenic heat sink systems with foamed boiling zone (Ustoichivost’ kriogennykh system teplosyema s vspenennoi zonoi kipeniya). In: Digest of SPA “Cryogenmash” scientific proceedings (Sbornik nauchnykh trudov NPO “Kriogenmash”). Balashikha, 1975, 30–42 (in Russ.).


Review

For citations:


Domashenko A.M., Tarasova E.Yu. DEVELOPMENT STAGES OF THE CRYOGENIC LAUNCH AND BENCH COMPLEXES OF THE ROCKET AND SPACE TECHNOLOGY. Alternative Energy and Ecology (ISJAEE). 2017;(19-21):49-73. (In Russ.)

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ISSN 1608-8298 (Print)