UDK 621.454.2 Doi: 10.31772/2587-6066-2018-19-3-469-481

1. Belyayev E. N., Chvanov V. K., Chervakov V. V. Matematicheskoye modelirovaniye rabochego protsessa zhidkostnykh raketnykh dvigateley [The mathematical modeling of working processes of liquid rocket engines]. Moscow, MAI Publ., 1999, 226 p.

2. Lebedinskiy E. N., Mosolov S. V., Kalmykov G. P. et al. Komp’yuternyye modeli zhidkostnykh raketnykh dvigateley [The computational momels of liquid rocket engines]. Moscow, Mashinostroenie Publ., 2009, 375 p.

3. Bradford J. E., Chararnia A., Germain B. St. REDTOP-2: Rocket Engine Design Tool Featuring Engine Performance, Weight, Cost, and Reliability. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2004-3514, 2004, 17 p.

4. Yang H. S., Park B. H., Yoon W. S. Modular Program for Conceptual Design of Liquid Rocket Engine System, Part I : Essential Components Design. Journal of the Korean Society for Aeronautical & Space Sciences. 2007, Vol. 35, No. 9, P. 805–815. DOI: 10.5139/JKSAS.2007.35.9.816.

5. Adzhyan A. P. [Features of the development of an oxidizing gas generator for a multi-mode single-chamber engine]. Trudy NPO Energomash. 2010, No. 27, P. 200–216 (In Russ.).

6. Adzhyan A. P., Rakhmanin V. F. [The evolution of progress gasgenerator of liquid rocket engine]. Dvigatel’. 2010, Vol. 2 (68), P. 13–15 (In Russ.).

7. Chen H.-Y., Liu H.-J., Chen J.-H. Forced start-up procedure of a staged combustion cycle engine. Journal of Aerospace Power. 2015, Vol. 30, Iss. 12, P. 3010–3016. DOI: 10.13224/j.cnki.jasp.2015.12.026.

8. Zhang X.-P., Ding F.-N. Starting process of oxidizer-rich staged combustion rocket engine. Journal of Propulsion Technology. 2004, Vol. 25, Iss.1, P. 82–85.

9. George P. S., Oscar B. Rocket Propulsion Elements, 8th ed. John Wiley & Sons Inc., 2010, 751 p.

10. Soon-Young Park, YoungJun Kim and Eun- Whan Jeong. Optimization of the Startup Sequence of a Liquid-propellant Rocket Engine. 7th european conference for aeronautics and space sciences (EUCASS). 2017. P. 17. DOI: 10.13009/EUCASS2017-293.

11. RD-120. Available at: http://www.npoenergomash.ru// dejatelnost/engines/rd120/rd120_4.html (accessed: 24.04.2016).

12. Al’bom konstruktsiy ZHRD [The album of design]. Ed. B. I. Katorgin, V. K. Chvanon. Khimki, KB NPO Energomash Publ., 1992, 259 p.

13. ZHRD RD-180. Available at: URL: http://lpre.de/energomash/RD-180/index.htm (accessed: 24.05.2018).

14. Belyayev E. N., Chervakov V. V. Matematicheskoye modelirovaniye ZHRD [The computational modelng of LRE]. Moscow, MAI Publ., 2009, 280 p.

15. Belyayev E. N., Vorob’yev A. G., Gnesin E. M. [Development of nonlinear mathematical model of liquid rocket engine working on stationary mode]. Trudy' MAI. 2014, Vol. 73 (In Russ.). Available at: http://www.mai.ru/science/trudy/published.php?ID=48537 (accessed: 15.03.2018).

16. Belyayev E. N., Chvanov V. K., Chervakov V. V. [Expiration of the two-phase gas-liquid mixture from the mixing head of the gas generator at the launch of the LRE]. Teplofizika vysokikh temperature. 2005, Vol. 43, No. 3, P. 446–451 (In Russ.).

17. Uollis G. Odnomernyye dvukhfaznyye techeniya [One-dimensional two-phases flow]. Moscow, Mir Publ., 1972, 440 p.

18. Katorgin B. I., CHvanov V. K., Belyayev E. N. et al. [The numerical modeling of modern LRE]. Dvigatel’. 2002, Vol. 4, P. 13–15 (In Russ.).

19. Shevyakov A. A., Kalnin V. M., Naumenkova N. V., Dyatlov V. G. Teoriya avtomaticheskogo upravleniya raketnymi dvigatelyami [Theory of automatic control of rocket engine]. Moscow, Mashinostroyeniye Publ., 1978, 288 p.

**Belayev Evgenyi Nikolaevich **– Cand. Sc., Docent, Department of Rocket engines, Faculty of Aircraft engines, Moscow Aviation Institute (National research university). E-mail: belyaev72@rambler.ru.

**Vorobyev Alexey Gennadievich **– Cand. Sc., Docent, Department of Rocket engines, Faculty of Aircraft engines, Moscow Aviation Institute (National research university). E-mail: formula1_av@mail.ru.