2017-1(22)

Nuclear, radiation and environmental safety

Article NameSafety of Perspective Spacecrafts with the Nuclear Power Installation
AuthorsO.A. Gubeladze*1, A.R. Gubeladze**2, S.M. Burdakov*3
Address

* Volgodonsk Engineering Technical Institute the branch of National Research Nuclear University “MEPhI”,
Lenin St., 73/94, Volgodonsk, Rostov region, Russia 347360
** Don State Technical University Gagarin square 1, Rostov-on-Don, Russia, 344000
 1e-mail: buba26021966@yandex.ru
ORCID iD: 0000-0001-6018-4989
WoS ResearcherID: F-6921-2017;
2e-mail: buba26021966@yandex.ru
ORCID iD: 0000-0002-6966-6391
WoS ResearcherID: F-7215-2017 ;
3 e-mail: SMBurdakov@mephi.ru
ORCID iD: 0000-0002-8599-6008
WoS ResearcherID: F-6903-2017

AbstractWork is carried out to ensure nuclear and radiation safety in the operation of advanced spacecrafts with nuclear power installations on board. The method of estimating the thermal effects of detachable currents can be used for probabilistic analysis of the safety of such devices.
Keywordsnuclear power station, spacecraft, atmospheric dense layers, thermal protection coating, detachable currents, cavity
LanguageRussian
References

 [1] Andreev P.V., Vasilkovskiy V.A. Kosmicheskaya yadernaya energetika: proshloe, nastoyashchee, budushchee [Space nuclear power: past, present, future]. AtomPRESSA [Atom PRESS], 2007, №15, pp. 1–2. (in Russian)

 [2] Zheleznyakov A.B. Tayny raketnykh katastrof: plata za proryv v kosmos [Mysteries of rocket accidents: a payment for break in space]. M. Pub. "Eksmo, Yauza" [Eksmo, Yauza publishing house], 2004, 544 p. (in Russian)

[3] Gubeladze O.A., Goncharov R.A. Zashchita vozvrashchaemoy chasti kosmicheskogo apparata [Protection of the returned part of the spacecraft]. Izvestiya vuzov. Severo-Kavkazsky region. Yestestvennye nauki. Prolozhenie [Scientific-educational and applied journal. University news of North-Caucasian region. Natural sciences series. Application], 2006, №1, ISSN 0321-3005, pp. 37–40. (in Russian)

[4] Krasnov N.F., Koshevoy V.N., Kalugin V.T. Aerodinamika otryvnykh techeniy [Aerodynamics of detachable currents]. M. Pub. "Vysshaya shkola" [High School publishing house], 1988, ISBN 5-06-001196-8, 351 p. (in Russian)

[5] Gubeladze O.A., Goncharov R.A., Levchenko E.M., Sakhabudinov R.V. Vliyanie defektov poverkhnosti korpusa letatelnogo apparata na teplovoy pogranichnyy sloy [Influence of case surface defects of the aircraft on a thermal interface]. Izvestiya vuzov. Severo-Kavkazsky region. Yestestvennye nauki. [Scientific-educational and applied journal. University news of North-Caucasian region. Natural sciences series], 2008, № 1, ISSN 0321-3005, pp. 28–29. (in Russian)

[6] Borodin R.V., Gubeladze O.A., Goncharov R.A. Osobennosti sverkhzvukovogo obtekaniya povrezhdennoy poverkhnosti vozvrashchaemoy chasti kosmicheskogo apparata [Features of a supersonic flow of the damaged surface of the returned part of the spacecraft]. Materialy VIII Mezhdunarodnogo foruma «Vysokie tekhnologii KhKhI v.» [Materials of the VIII International forum "High Technologies in XXI"]. M. Pub. CJSC "Mavr" [CJSC "Mavr" publishing house], 2007, pp. 51–52. (in Russian)

[7] Avery D.E., Kerr P.A., Wieting A.R. Experimental aerodynamic heating to simulated Shuttle tiles. CITEWEB.INFO — WORLDWEB CITATION DATABASE, 1983. Available at: http://citeweb.info/19850194847 (in Russian)

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