Skip to main content
Log in

Experimental Study of the International Space Station Contamination by Its Orientation Thrusters Jets

  • Topical Issue Two-Phase Systems Italy
  • Published:
Microgravity Science and Technology Aims and scope Submit manuscript

Abstract

This paper deals with modeling in a vacuum chamber of the International Space Station (ISS) contamination processes caused by its orientation thrusters (OT), namely with experimental study of joint ejection of gas and near-wall liquid film from a supersonic nozzle into vacuum. The description of experimental setup and measurement techniques is presented in the paper. Local parameters of near-wall liquid film—its thickness and velocity at the nozzle outlet are measured. It is shown that film thickness and velocity do not depend on nozzle orientation, i.e. measurement results are not influenced by gravity. The structure of droplet phase flow arising behind the exit cross-section of a supersonic nozzle in vacuum under microgravity conditions is obtained. Results are confirmed by three independent measurement techniques. Appearance of droplet phase backflows which cause contamination of space station exterior is shown. The way of space station contamination minimization is suggested. It is shown that using of special gas-dynamical protective devices—screens, mounted at the exit part of a nozzle, allows to reduce phenomenon of contaminating back flows significantly. Carried out space experiment ≪Kromka≫ showed good correspondence of real experiment results with results of model experiment. It also approved the suggested way of ISS contamination minimization.

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.

Similar content being viewed by others

References

  • Afanasiev, I.: Kovarnaya ≪Kromka≫ // Novosti Kosmonavtiki, No.4, pp. 15–16 (in Russian) (2004)

  • Dettleff, G., Plahn, K.: Experimental investigation of fully expanding free jets and plume. Proc. of the 21st Int. Symp. RGD. 1, 607–614 (1998)

    Google Scholar 

  • Gerasimov, Yu.I., Krylov, A.N., Sokolova, S.P., Prikhodko, V.G., Yarygin, V.N., Yarygin, I.V., Rebrov, S.G., Buryak, A.K.: Gas-dynamic aspects of the contamination problem at the International space station. 2. On board experiments. Thermophysics and Aeromechanics. 10(4), 555–565 (2003)

    Google Scholar 

  • Gerasimov, Yu.I., Yarygin, V.N.: Problems of gas-dynamical and contaminating effect of exhaust plumes of orientation thrusters on space vehicles and space stations. Proc. of the 25th Int. Symp. RGD25, 805–811 (2007)

  • Prikhodko, V.G., Khramov, G.A., Yarygin, V.N.: A large-scale cryogenic vacuum plant for gas-dynamics research. Instrum. Exp. Tech. 39(2), 309–311 (1996)

    Google Scholar 

  • Prikhodko, V., Yarygin, I., Yarygin, V.: Mass transfer and friction in near-wall film flows in conditions of high-velocity co-current gas flow. Microgravity Sci. Technol. 21(1), S277–S281 (2009)

    Article  Google Scholar 

  • Rebrov, S., Gerasimov, Y.: Investigation of the Contamination Properties of Bipropellant Thrusters. AIAA Paper No. 2001-2818, AIAA 35th Thermophysics Conference, 11–14 June 2001, Anaheim, California (2001)

  • Serov, A.F., Kotov, S.V., Nazarov, A.D., Pavlenko, A.N., Pecherkin, N.I., Chehovich, V.Yu.: Capacitive meter of local thickness of liquid films. Instrum. Exp. Tech. 40(1), 136–139 (1997)

    Google Scholar 

  • Trinks, H.: Experimental Investigation on the Exhaust Plume Flow Fields of Various Small Bipropellant and Monopropellant Thrusters. AIAA Paper No. 87-1607, AIAA 22nd Thermophysics Conference, June 8–10, Honolulu, Hawaii (1987)

    Google Scholar 

  • Trinks, H., Kaelsch, I.: Exhaust Plume Effects of Small Thrusters on Spacecraft. AIAA Paper No. 87-1603, AIAA 22nd Thermophysics Conference, June 8–10, Honolulu, Hawaii (1987)

  • Yarygin, I.V., Levchenko, V.F.: Measurement and calculation of thickness and velocity of a near-wall liquid film at motion with a co-current gas flow in a supersonic nozzle. Proc. XII Int. Conf. on the Methods of Aerophysical Research ICMAR.—Part 4, 310–314 (2004)

  • Yarygin, V.N., Prikhodko, V.G., Yarygin, I.V.: Jet expansion of gas with near-wall liquid film from nozzle into vacuum. Microgravity Sci. Technol. 21(1), S271–S275 (2009)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Vyacheslav Yarygin.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Yarygin, V., Gerasimov, Y., Krylov, A. et al. Experimental Study of the International Space Station Contamination by Its Orientation Thrusters Jets. Microgravity Sci. Technol. 23 (Suppl 1), 15–23 (2011). https://doi.org/10.1007/s12217-011-9266-5

Download citation

  • Received:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12217-011-9266-5

Keywords

Navigation