Skip to main content
Log in

Operation of a gas generator controlled by supplying a gaseous oxidizer

  • Published:
Combustion, Explosion, and Shock Waves Aims and scope

Abstract

The possibility of arranging a gas generator with the heat-release process being controlled by supplying a gaseous oxidizer is experimentally checked. Gaseous hydrogen, liquid gasoline, and solid hexamethylene tetramine (solidified alcohol) is used as a fuel. The gas generator with a proposed configuration is demonstrated to ensure stable operation during combustion of various fuels; the pressure in the gas-generator combustion chamber does not exceed the pressure of oxidizer supply and clearly correlates with variations of the oxidizer mass flow. Quasi-steady calculations allow determining all parameters of the process, including those that are not measured in the experiment. In particular, the temperature of combustion products is found to be 600–1900 K, and the gas generator forms a high-temperature mixture containing a non-reacted fuel (the air-to-fuel ratio is α = 0.55–2.30).

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

  1. M. I. Sokolovskii and V. I. Petrenko (eds.), Controlled Energetic Facilities Operating on Solid Propellants [in Russian], Mashinostroenie, Moscow (2003).

    Google Scholar 

  2. A. A. Shishkov and B. V. Rumyantsev, Gas Generators for Rocket Systems [in Russian], Mashinostroenie, Moscow (1981).

    Google Scholar 

  3. B. V. Orlov, G. Yu. Mazing, A. L. Reidel, M. N. Stepanov, and Yu. I. Tolcheev, Fundamentals of Design of Air-Breathing Rocket Engines for Unmanned Flying Vehicles [in Russian], Mashinostroenie, Moscow (1967).

    Google Scholar 

  4. R. E. Sorkin, Theory of Intra-Chamber Processes in Solid-Propellant Rocket Systems: Internal Ballistics [in Russian], Nauka, Moscow (1983).

    Google Scholar 

  5. L. G. Golovkov, Hybrid Rocket Engines [in Russian], Voenizdat, Moscow (1976).

    Google Scholar 

  6. E. V. Gerts, Calculation of Pressure-Controlled Drives [in Russian], Mashinostroenie, Moscow (1975).

    Google Scholar 

  7. N. M. Belyaev, Thermodynamics of a Variable Amount of Gas [in Russian], Dnepropetrovsk State University, Dnepropetrovsk (1981).

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to V. I. Zvegintsev.

Additional information

__________

Translated from Fizika Goreniya i Vzryva, Vol. 44, No. 6, pp. 18–25, November–December, 2008.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Vnuchkov, D.A., Zvegintsev, V.I., Nalivaichenko, D.G. et al. Operation of a gas generator controlled by supplying a gaseous oxidizer. Combust Explos Shock Waves 44, 632–638 (2008). https://doi.org/10.1007/s10573-008-0097-7

Download citation

  • Received:

  • Revised:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s10573-008-0097-7

Key words

Navigation