Сибирский государственный университет
науки и технологий имени академика М.Ф. Решетнева

1. Salked R., Beichel R. Reusable one-stage-to orbit shuttles: bright energy propects. Astronaut. Aeronaut. 11, 1973. P. 6–48.
2. Belyaev E. N., Vorob’yev А. G. [Influence of filling processes of gas generator mixing heads on the dynamics of a non-starter launch of a liquid rocket engine]. Siberian Journal of Science and Tech-nology. 2018, Vol. 19, No. 3, P. 469–481. Doi: 10.31772/2587-6066-2018-19-3-469-481. (In Russ.)
3. Belyakov V.A., Vasilevskiy D. O. [Perspective circuit solutions of liquid rocket engine by expanded cycle]. Vestnik PNIPU. Aerospace science. 2019, Vol. 58, P. 69–86. Doi: 10.15593/2224-9982/2019-58-06. (In Russ.)
4. Gusev V. N., Semenov V. I., Storozhenko I. G. [Three-Component two-mode main engine for aerospace systems and new-generation launch vehicles]. Alternative energy and technology. 2008, No. 3 (59), P. 36–41. (In Russ.)
5. Goncharov G. I., Goncharov N. With., Replevy I. V. et al. Experimental’nyj Zhidkostnoj raketnij dvigatel’ s dozhiganiem [Experimental liquid-propellant rocket engine with afterburning]. Pat RF. No. 2065068, 1994.
6. Goncharov G. I., Replevy I. V., Orlov V. A. et al. Trekh komponentnyj Zhidkostnoj raketnij dvigatel’ [Three-component liquid propellant rocket engine]. Pat RF. No. 2065985, 1994.
7. Gorokhov V. D., Milovanov A. G. Trekh komponentnyj Zhidkostnoj raketnij dvigatel’ [Three-component liquid propellant rocket engine]. Pat RF. No. 2575238, 2014.
8. Semenov V. V., Ivanov I. E., Sorokin V. A. et al. Vysotnoe Soplo Lavalya [High-altitude Laval nozzle]. Pat RF. No. 125262, 2013.
9. Abashev V. M., Demidov A. S., Eremkin I. V. et al. [Temperature stresses in cylindrical shells made of carbon fibers and the contact problem of heat exchange]. Vestnik MAI. 2017, Vol. 24, No. 4, P. 7–13. (In Russ.)
10. Girshfelder D., Curtis Ch., Byrd R. Molekularnaya teoria gazov i zhidkostej [Molecular theory of gases and liquids]. Moscow, Foreign literature publ., 1961, 931 p.
11. Bretschneider S. Svojstva gazov i zhidkostej [Properties of gases and liquids]. Moscow, Chemistry publ., 1936, 536 p.
12. Gidaspov V. Yu. [Numerical simulation of a chemically nonequilibrium flow in a liquid rocket engine nozzle]. Vestnik MAI. 2013, Vol. 20, No. 2, P. 90–95. (In Russ.)
13. Piunov V. Yu., Nazarov V. P., Kolomentsev A. I. [Improving the energy characteristics of oxygen-hydrogen liquid-propellant rocket engines of upper stages of methods for optimizing design schemes]. Vestnik MAI. 2017, Vol. 24, No. 3, P. 23–33. (In Russ.)
14. Orlin S. A., Orlov A.V. [Increasing the specific impulse of liquid rocket engines running on oxygen + kerosene fuel by adding hydrogen to the combustion chamber]. Engineering journal: science and innovation. 2019, No. 11, P. 23–33. Doi: http://dx.doi. org/10.18698/2308-6033-2019-11-1935. (In Russ.)
15. Belyaev E. N., Vorob’yev A. G. Energeticheskaya uvyazka parametrov zhidkostnogo raketnogo dvigatelya [Energy coupling of parameters of a liquid rocket engine]. Moscow, MAI publ., 2016, 68 p.
16. Belyaev E. N., Vorob’yev A. G., Nascimento L. B. et al. [Problematic issues of energy coupling of parameters of liquid rocket engines]. Trudy' MAI. 2013, Vol. 71 Available at: https://mai.ru/ upload/iblock/382/382669ab36066d251d57dd531a45cd9f.pdf (accessed: 06.03.2020). (In Russ.)
17. Kozlov A. A., Novikov V. N., Soloviev E. V. Sistema pitaniya I upravleniya zhidkostych raketnyh dvigatelnyh ustanovok [Power supply and control systems for liquid rocket propulsion systems]. Moscow, Mashinostroenie publ., 1988, 347 p.
18. Nesterov V. E., Rudakov V. B., Makarov V. I. [Analysis of the main tasks of experimental testing of a reusable rocket and space system]. Vestnik MAI. 2013, Vol. 20, No. 5, P. 77–85. (In Russ.).