Previous Page  17 / 18 Next Page
Information
Show Menu
Previous Page 17 / 18 Next Page
Page Background

С.Л. Финогенов, А.И. Коломенцев

82

ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. Машиностроение. 2017. № 2

REFERENCES

[1] Grilikhes V.A., Matveev V.M., Poluektov V.P. Solnechnye vysokotemperaturnye istochniki

tepla dlya kosmicheskikh apparatov [Solar high-temperature thermal source for spacecraft].

Moscow, Mashinostroenie Publ., 1975. 248 p.

[2] Shoji J.M., Frye P.E. Solar thermal propulsion for orbit transfer.

AIAA Paper

, 1988,

no. 3171.

[3] Kudrin O.I. Solnechnye vysokotemperaturnye kosmicheskie energodvigatel'nye ustanovki

[Solar high-temperature spacecraft propulsion system]. Moscow, Mashinostroenie Publ., 1987.

247 p.

[4] Caveny L.H., ed. Orbit-raising and maneuvering propulsion: research status and needs.

In Ser.: Progress in astronautics and aeronautics. Vol. 89. New York, American Institute of

Aeronautics and Astronautics, 1988. 454 p. (Russ. ed.: Kosmicheskie dvigateli: sostoyanie i

perspektivy. Moscow, Mir Publ., 1988. 454 p.)

[5] Finogenov S.L., Kolomentsev A.I., Kudrin O.I. Kosmicheskie dvigateli, ispol'zuyushchie

solnechnuyu i khimicheskuyu energiyu [Spacecraft engines using solar and chemical energy].

Moscow, MAI Publ., 2016. 100 p.

[6] Leenders H.C.M., Zandbergen B.T.C. Development of a solar thermal thrusters system.

59th IAC Congress

. Glasgow, Scotland, 2008. Paper IAC-08- D1.1.01.

[7] Akimov V.N., Arkhangel'skiy N.I., Koroteev A.S., Kuz'min E.P. Solar propulsion system

with arcjet thermal accumulator and working medium post-combustion.

Polet

[Flight], 1999,

no. 2, pp. 20–28 (in Russ.).

[8] Koroteev A.S. Conception of solar propulsion system with arcjet thermal accumulator and

working medium post-combustion.

Vestnik MAI

, 2000, vol. 7, no. 1, pp. 60–67 (in Russ.).

[9] Scharfe D., Young M. A study of solar thermal propulsion system enhancement via ther-

mal storage and thermal-electric conversion.

Proceedings of the 59th JANNAF Joint Subcom-

mittee Meeting

. Colorado Springs, USA, 2010.

[10] Finogenov S.L., Kudrin O.I. Consistency principle in solar thermal rocket engine engi-

neering.

Sistemnyy analiz v tekhnike. Tematicheskiy sbornik nauchnykh trudov. Vyp. 8

[System

analysis in technics. Subject collection of thesises]. Moscow, Vuzovskaya kniga Publ., 2005,

pp. 36–80.

[11] Finogenov S.L., Kolomentsev A.I. Parameters selection of solar thermal rocket engine

under flight time limitation.

Vestnik MAI

, 2016, vol. 23, no. 3, pp. 58–68 (in Russ.).

[12] Shimizu M. et al. Solar thermal thruster made of single crystal molybdenum.

Acta Astro-

nautica

, 1997, vol. 41, no. 1, pp. 23–28.

[13] Fiot D., Estublier D. Solar thermal propulsion.

6th International Symposium on Propul-

sion for Space Transportation: Propulsion for Space Transportation of the XXIst Century

. 2002.

Versailles, France. Paper № S36.1.

[14] Kvasnikov A.V., Kudrin O.I., Mel'nikov M.V. [Radiant and solar energy laboratory for

exploration of processes in high-temperature equipment].

Dokl. Vsesoyuz. konf. po

ispol'zovaniyu solnechnoy energii

[Proc. Russ. conf. on solar energy usage]. Moscow, VNIIT

Publ., 1969, pp. 297–343.

[15] Safranovich V.F., Emdin L.M. Marshevye dvigateli kosmicheskikh apparatov. Vybor tipa i

parametrov [Spacecraft cruise engines. Choice of type and parameters]. Moscow, Mashinostroenie

Publ., 1980. 240 p.