Skip to main content
Log in

MODELING OF SPACE VEHICLE ORIENTATION THRUSTER JETS IN VACUUM CHAMBERS

  • Published:
Journal of Applied Mechanics and Technical Physics Aims and scope

Abstract

This paper presents a brief overview of experimental studies performed at the Institute of Thermophysics of the Siberian Branch of the Russian Academy of Sciences to model jets of low-thrust liquid rocket engines used as control and orientation thrusters of spacecrafts, including the International Space Station. Modeling criteria are formulated for the parameters of both the gas flow and the near-wall liquid film used for nozzle cooling. The experimental setup, diagnostic methods, and experimental results on the interaction of the near-wall liquid film with co-current gas flow inside the supersonic nozzle and during jet expansion into vacuum are described. The problem of minimizing backflows leading to contamination of the spacecraft external surfaces is discussed.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8

Similar content being viewed by others

REFERENCES

  1. I. Afanas’ev, “Insidious ‘Kromka’," Novosti Kosm., No. 4, 15–16 (2004).

  2. Yu. I. Gerasimov and V. N. Yarygin, “Gas-Dynamical Protective Devices for Orientation Thrusters of Space Vehicles and Orbital Stations. Conceptual Design, Model and On-Orbit Experiments," Phys.-Chem. Kinet. Gas Dyn. 17 (4) (2016); http://chemphys.edu.ru/issues/2016-17-4/articles/671/.

  3. Yu. I. Gerasimov, “Similarity Parameters of the Problem of Interaction of a Freely Expanding Jet with a Plate," Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza 10 (2), 169–173 (1981).

  4. Yu. I. Gerasimov, N. G. Gorchakova, S. A. Palopezhentsev, and V. N. Yarygin, “Modeling of the Parameters of High Off-Design Jet Flow in Vacuum Chambers," in Proc. 9th All-Union. Conf. on the Dynamics of Rarefied Gases, Sverdlovsk, June 23–25, 1987(Ural Polytech. Inst., Sverdlovsk, 1988), Vol. 3, pp. 144–151.

  5. V. N. Yarygin, V. G. Prikhodko, I. V. Yarygin, and A. D. Nazarov, “Interfacial Friction and Mass Transfer at Gas Flow into Vacuum through a Nozzle with a Near-Wall Liquid Film," Teplofiz. Aeromekh. 20 (6), 759–768 (2013) [Thermophys. Aeromech.20 (6), 739–747 (2013); https://doi.org/10.1134/S0869864313060115].

  6. V. G. Prikhodko, G. A. Khramov, and V. N. Yarygin, “Large-Scale Cryogenic-Vacuum Setup for Studying Gas-Dynamic Processes," Prib. Tekh. Eksp., No. 2, 162–164 (1996).

  7. V. N. Yarygin, V. G. Prikhodko, and I. V. Yarygin “Features of the Formation and Evaporation of Near-Wall Liquid Films when Flowing from the Nozzle into Vacuum," Pikl. Mekh. Tekh Fiz. 59(5), 39–47 (2018) [J. Appl. Mech. Tech. Phys. 59 (5), 801–808 (2018); https://doi.org/10.1134/S002189441805005X].

  8. V. N. Yarygin, V. G. Prikhodko, I. V. Yarygin, and Yu. N. Vyazov, “Near-Wall Liquid Film Ejection with Co-Current Gas Flow from Nozzle into Vacuum," Vacuum 109, 401–404 (2014).

  9. V. G. Prikhodko, I. V. Yarygin, and Yu. N. Vyazov, “Spectrophotometry Technique for Droplet Phase Spatial Distribution Measurements in Gas-Droplet Flow behind a Supersonic Nozzle in a Vacuum," Interfac. Phenom. Heat Transf. 7 (2), 105–111 (2019).

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to V. N. Yarygin.

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Yarygin, V.N., Prikhodko, V.G. & Yarygin, I.V. MODELING OF SPACE VEHICLE ORIENTATION THRUSTER JETS IN VACUUM CHAMBERS. J Appl Mech Tech Phy 61, 798–806 (2020). https://doi.org/10.1134/S0021894420050144

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S0021894420050144

Keywords

Navigation