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Analysis of Energy Capabilities of Acceleration of Massive Projectiles by Gas-Dynamic Methods

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Abstract

The energy capabilities of acceleration devices are theoretically analyzed, including various ramjet-in-tube options for gas-dynamic acceleration of massive (1 to 40 kg) projectiles under ground conditions up to velocities of 2–3 km/s. Simple quasi-one-dimensional models for a perfect gas are used in the computations. It is demonstrated that the use of a ramjet-in-tube accelerator with a closed exit allows the velocities of acceleration of massive projectiles to be increased to 3 km/s, which is twice greater than the values that can be obtained with available gunpowder-based methods.

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References

  1. O. G. Agoshkov, A. V. Belov, E. M. Beletskii, and Yu. L. Vyashchenko, Artillery Weapons: Tutorial (Balt. Gos. Tekh. Univ., St. Petersburg, 2004) [in Russian].

    Google Scholar 

  2. V. F. Zakharenkov, Internal Ballistics and Automation of Artillery Weapon Design: Tutorial (Balt. Gos. Tekh. Univ., St. Petersburg, 2010) [in Russian].

    Google Scholar 

  3. V. I. Blinov and V. G. Larin, “Method of High-Speed Acceleration of Projectiles and Device for Implementation of the Method,” RF Patent No. 2311604, MPK F 41 F 1/00, Publ. 05.11.2006.

    Google Scholar 

  4. Yu. S. Komratov, V. A. Kukis, V. F. Komarov, and Yu. A. Chikunov, “Method of Increasing the Flight Range of the Projectile and Device for Implementation of the Method,” RF Patent No. 2457418, MPK F 41 A 1/06, F 41 A 21/28, Publ. 12.23.2010.

    Google Scholar 

  5. P. P. McDermott, “Multivalve Hypervelocity Launcher (MHL),” USA Patent No. 7775148, IPC F 41 A 1/02, Publ. 08.18.2010.

    Google Scholar 

  6. A. Hertzberg, A. P. Bruckner, and D. W. Bogdanoff, “Ram Accelerator: A New Chemical Method for Accelerating Projectiles to Ultrahigh Velocities,” AIAA J. 26 (2), 195–203 (1988).

    Article  ADS  Google Scholar 

  7. A. P. Bruckner, C. Knowlen, A. Hertzberg, and D. W. Bogdanoff, “Operational Characteristics of the Thermally Choked Ram Accelerator,” J. Propulsion Power 7 (5), 828–836 (1991).

    Article  Google Scholar 

  8. A. Hertzberg, A. P. Bruckner, and D. W. Bogdanoff, “Apparatus and Method for the Acceleration of Projectiles to Hypervelocity,” USA Patent No. 4938112, IPC F 41 A 1/02, Publ. 07.03.1990.

    Google Scholar 

  9. A. E. Kull, E. A. Burnham, C. Knowlen, et al., “Experimental Studies of Superdetonative Ram Accelerator Modes,” AIAA Paper No. 89-2632 (1989).

    Book  Google Scholar 

  10. G. Chew, C. Knowlen, E. A. Burnham, et al., “Experiments on Hypersonic Ramjet Propulsion Cycles Using a Ram Accelerator,” AIAA Paper No. 91-2489 (1991).

    Book  Google Scholar 

  11. A. P. Bruckner, “The Ram Accelerator: A Technology Overview,” AIAA Paper No. 2002-1014 (2002).

    Google Scholar 

  12. A. J. Higgins, “Ram Accelerators: Outstanding Issues and New Directions,” J. Propulsion Power 22 (6), 1170–1187 (2006).

    Article  MathSciNet  Google Scholar 

  13. P. Bauer and T. Bengherbia, “The Ram Accelerator in Subdetonative Propulsion Mode: Analytical and Numerical Modeling and Simulation,” in Hypervelocity Launchers (Springer, Switzerland, 2016), pp. 165–203. (Shock Wave Sci. Technol. Reference Library, Vol. 10.)

    Chapter  Google Scholar 

  14. A. Hertzberg, A. P. Bruckner, and C. Knowlen, “Experimental Investigation of Ram Accelerator Propulsion Modes,” Shock Waves, No. 3, 17–25 (1991).

    Google Scholar 

  15. G. Legendre and S. Catoire, “Ram Accelerator in 90 mm Calibre. First Results Concerning Scale Effects in the Thermally Choked Propulsion Mode,” in Proc. of the 13th Int. Symp. on Ballistics, Stockholm (Sweden), June 1–3, 1992.

    Google Scholar 

  16. D. L. Kruczynski, A. W. Horst, and T. C. Minor, “Experimental Demonstration of a 120-mm Ram Accelerator,” Technical Report Army Res. Lab. No. ARL-TR-1237 (1996).

    Google Scholar 

  17. N. M. Belyaev, Thermodynamics of a Variable Amount of a Gas: Tutorial (Dnepropetr. Gos. Univ., Dnepropetrovsk, 1981) [in Russian].

    Google Scholar 

  18. A. Hertzberg, A. P. Bruckner, C. Knowlen, and K. A. McFall, “Method and Apparatus for Zero Velocity Start Ram Acceleration,” USA Patent No. 5097743, IPC F 41 A 1/02, F 41 F 1/00, Publ. 03.24.1992.

    Google Scholar 

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Correspondence to V. I. Zvegintsev.

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Original Russian Text © V.M. Fomin, V.I. Zvegintsev, E.Ya. Braguntsov.

Translated from Prikladnaya Mekhanika i Tekhnicheskaya Fizika, Vol. 60, No. 3, pp. 15–28, May–June, 2019.

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Fomin, V.M., Zvegintsev, V.I. & Braguntsov, E.Y. Analysis of Energy Capabilities of Acceleration of Massive Projectiles by Gas-Dynamic Methods. J Appl Mech Tech Phy 60, 411–423 (2019). https://doi.org/10.1134/S0021894419030027

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  • DOI: https://doi.org/10.1134/S0021894419030027

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