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REFERENCES

[1] NASA Stennis Space Сenter test technologies branch activites. Wanda M. Solano.

Stennis Space Center:

3rd International Hydrogen Peroxide Propulsion Conference.

13–15 November 2000.

[2] Wright Andrew B., Elsasser Jason E., Hudson M. Keith, Wright Ann M. Optical

studies of combustion chamber flame in a hybrid rocket motor. University of Arkansas

at Little Rock (UALR).

Journal of Pyrotechnics

, 2005, iss. 21.

[3] Hudson M. Keith, Shanks Robert B., Snider Dallas H., Lindquist Diana M., Luchini

Chris, Rooke Sterling. UV, visible and infrared spectral emissions in hybrid rocket

plumes. University of Arkansas at Little Rock (UALR).

International Journal of

Turbo and Jet Engines

. March 1998, vol. 15, iss. 1.

[4] Gafurov R.A., Solov’ev V.V. Diagnostika vnutrikamernykh protsessov v

energeticheskikh ustanovkakh [Diagnosis of intrachamber processes in power plants].

Moscow, Mashinostroenie Publ., 1991. 272 p.

[5] Tejwani Gopal D., Van Dyke David B., Bircher Felix E., Gardner Donald G. Emission

spectra of selected SSME elements and materials. Stennis Space Center:

NASA

Reference publication

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[6] Golovin Yu.M., Zavelevich F.S., Kuchin A.P., Matsitskiy Yu.P., Moshkin

K.B., Romanovskiy A.S. Spectrophotometric Method for Liquid Rocket Engine

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Thermophysics], 2002, Belarus (in Russ.).

[7] Tejwani G.D. Shuttle main engine health monitoring with exhaust plume emission

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[8] Whitaker K.W. Analyzing rocket plume spectral data with neural networks for

condition monitoring. The University of Alabama:

RTO AVT Course on “Intelligent

Systems for Aeronautics”

in Rhode-Saint-Gen`ese, Belgium. 13–17 May 2002.

[9] Madzsar G.C. Determination of alloy content from plume spectral measurements.

Lewis Research Center:

27th Joint Propulsion Conference cosponsored by AIAA,

SAE, ASME, and ASEE,

Sacramento, California. 24–27 June 1991.

[10] Zavelevich F.S., Golovin Yu.M., Matsitskiy Yu.P., Moshkin K.B. Spectrophotometric

Method for Quantitative Evaluation of LRE Material Ablation. 19 Vseross. nauch.-

tekh. konf. “Vysokoskorostnaya fotografiya i fotonika” [High-Speed Photography

and Photonics]. Moscow, 2001(in Russ.).

[11] The Program for Calculating the Thermodynamic Functions and Properties of the

Reaction Mixture at Equilibrium. Report on: Study of High-Temperature Processes

in Engines and Power Plants. Kazan’, KAI, 1977 (in Russ.).

[12] Zavelevich F.S., Ushakov N.N. Certificate of State Registration of the Software

No. 2014615940. Program for Calculating the Interaction of the Propulsion Exhaust

Jet, Operating at Different Propellant with the Atmosphere (STR-ECO). Application

No. 2014612996. Date of receipt of application 07.04.2014, State registration date

06.06.2014.

Статья поступила в редакцию 9.09.2014

Травников Роман Игоревич — ведущий инженер ГНЦ “Исследовательский центр

имени М.В. Келдыша”. Автор 47 научных работ в области исследований тепловых,

электроракетных двигателей и энергоустановок летательных аппаратов.

Исследовательский центр имени М.В. Келдыша, Российская Федерация, 125438,

Москва, Онежская ул., д. 8.

Travnikov R.I. — a senior engineer of the Keldysh Research Center, author of 47

publications in the fields of liquid, solid and electrical rocket engines.

Keldysh Research Center, Onezhskaya ul. 8, Moscow, 125438 Russian Federation.

ISSN 0236-3941. Вестник МГТУ им. Н.Э. Баумана. Сер. “Машиностроение” 2015. № 4 47