Reasons determination of liquid rocket engine damage situations using engine experiment data

1Pron', LV, 2Samokhvalov, SA
1Oles Honchar Dnipro National University, Dnipro, Ukraine
2Oles Honchar Dnipro National University, Dnipro, Ukraine
Kosm. nauka tehnol. 2002, 8 ;(Supplement1):040-045
Publication Language: Russian
An attempt of the statistical determination of disrepair type on the basis of the disrepair localization using a vector of the special selected parameters has been done, this disrepair resulted from the damage situation.
1. Luarsabov K. A., Pron' L. V., Serdyuk A. V. In-Flight Testing of Liquid-Fuel Rocket Engines. (Moscow, 1997) [in Russian].
2. Makhin V. A., Milenko N. P., Pron’ L. V. Theoretical Principles of the Experimental Depletion of Liquid Rocket Engines. (Moscow, 1973) [in Russian].
3. Fu K. S. Sequential Methods in Pattern Recognition and Machine Learning. (Moscow, 1971) [in Russian].
4. Gnedov G. M., Rosenbauli O. B., Shumov Iu. A. Design of rocket control systems, 224 p. (Mashinostroenie, Moscow, 1975) [in Russian].
5. Korn G. A., Korn Th. M. Mathematical handbook for scientists and engineers: definitions, theorems and formulas for reference and review. (Nauka, Moscow, 1974) [in Russian].

6. Volkov E. B., Sudakov R. S., Syritsyn T. A. The theoretical principles of reliability of rocket motors, 400 p. (Mashinostroenie, Moscow, 1974) [in Russian].