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The Possibility of the Use of High Explosive Layers in Ram Accelerators

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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The possibility of the use a high energetic solid material in a ram accelerator is discussed in this paper. First, some facts about multiphase combustion observed in ram accelerators are presented. While the core problem of using high explosive in supersonic propulsion is fast combustion, the first stage of work consisted of measuring ignition delays of selected high explosives. The ignition is triggered by a passing detonation wave. The experimental results proved that those materials can be applied to the ram accelerator and PETN has been selected as the best material. Next, a numerical model of ignition and combustion of a high explosive layer in a ram accelerator has been created and applied in numerical simulations. The obtained results allowed estimations of thrust enhancement and parametric analysis of the influence of some parameters on performances of the device. It was found that use of layers of high explosive can increase the generated thrust by about 10%. However this depends on such parameters as the speed of the projectile, initial pressure of the gaseous mixture, and the geometry of the projectile.
Słowa kluczowe
Rocznik
Strony
149--171
Opis fizyczny
Bibliogr. 28 poz., rys., tab.
Twórcy
autor
autor
  • Warsaw University of Technology, Faculty of Power and Aeronautical Engineering, ul. Nowowiejska 21/25, 00-665 Warsaw.
Bibliografia
  • [1] Hertzberg A.P., Bruckner D., Bogdanoff D.W.: Ram Accelerator: A New Chemical Method for Accelerating Projectiles to Ultrahigh Velocities. AIAA Journal, 26, No. 2, (1998), pp. 195-203
  • [2] Bogdanoff, D.W.: Ram Accelerator Direct Space Launch System: New Concepts. J. of Prop. and Power, 8, No. 2, (1992)
  • [3] Ingignoli W., Veyssiere .B, Khasainov B.A.: On the Possibility to Modify the Performances of Propellant Mixtures Used in RAMAC by Addition of Metallic Particles. Proceedings of Fourth International Workshop on RAM Accelerators, Poitiers, (1999)
  • [4] Leblanc J.E., Lefebvre M.H., Fujiwara T.: Detailed Flowfields of a RAMAC Device in H2-O2 Full Chemistry. Shock Waves, 6, (1996)
  • [5] Takayama K., Sasoh A. (Eds.): Ram Accelerators. Berlin, Heidelberg, New York, 1997, Springer-Verlag
  • [6] Yungster, S.,Bruckner, A.P.: Computational Studies of a Superdetonative Ram Accelerator Mode. J. of Prop. and Power, 8, No. 2, (1992)
  • [7] Brandeis, J.: Ram Accelerator Utilizing Active Projectile. J. of Prop. and Power, 12, No. 2, (1996)
  • [8] Higgins A.J.: Ram Accelerators: Outstanding Issues and New Directions. J. of Prop. and Power, 22, No. 6, (2006)
  • [9] Veyssiere, B.: Detonations in Gas-Particle Mixtures. J. of Prop. and Power, 22, No. 6, (2006)
  • [10] Seiler G., Patz G., Smeets G., Srulijes J.: Ongoing of Superdetonative Ram Acceleration Experiments in ISL’s Ramac 30. Proceedings of Fourth International Workshop on RAM Accelerators, Poitiers, (1999)
  • [11] Catoire, L., Legendre, J.-F.,Giraud, M.: Kinetic Model for Aluminum-Sensitized Ram Accelerator Combustion. J. of Prop. and Power, 19, No. 2, (2003)
  • [12] Rodenberger C.A., Sawyer M.L.: Fast Burning Rate in Thin Film Propellants. AIAA Journal, 10, (1972).
  • [13] Carrier G., Fendell F., Wu F.: Projectile Acceleration in a Solid-Propellant-Lined Tube. Comb. Sci. & Techn., 104, (1995)
  • [14] Wolański P., Kobiera A.: Ignition of Liquid and Dust Fuel Layer by Hydrogen-Oxygen Detonation. Proceedings of the 18th International Colloquium on the Dynamics of Explosions and Reactive Systems, Washington, (2001).
  • [15] Kobiera A., Wolanski P.: Ignition of liquid and dust fuel layers by gaseous detonation. Shock Waves, 12, No. 5, (2003).
  • [16] Cudziło S., Maranda A., Nowaczewski J., Trębiński R., Trzciński W.A.: Wojskowe materiały wybuchowe. Czestochowa 2000, WWMiIM Politechniki Częstochowskiej
  • [17] Smoleński D.: Spalanie materiałów wybuchowych. Warszawa 1979, Wydawnictwo MON.
  • [18] Urbański T.: Chemistry and technology of explosives. Warsaw 1964, PWN
  • [19] Gordon S., McBride B.J., Zeleznik F.J.: Computer Program for Calculation or Complex Chemical Equilibrium Composition, Rocket Performance, Incident and Reflected Shocks, and Chapman Jouguet Detonation. NASA Report SP-273, (1973)
  • [20] Kobiera A., Wolański P.: Modelling of ignition of PETN layer by gaseous detonation. Arch. Combust., 23, No 3-4, (2003)
  • [21] Wolański P., Kobiera A.: Experimental and numerical research on interaction between gaseous detonation and solid explosive. Proceedings of 19th International Colloquium on the Dynamics of Explosions and Reactive Systems, Hakone, (2003)
  • [22] Kobiera A., Wolanski P.: Combustion of high explosive layers ignited by detonation waves. Arch. Combust., 24, No. 1-2 (2004)
  • [23] Dyne B.R., Heinricht, J.C.: Finite Element Analysis of the Scramaccelerator with Hydrogen-Oxygen Combustion. J. of Prop. and Power, 12, No. 2, (1996).
  • [24] Kobiera A., Wolanski P.: Simulation of Ram Accelerator with PETN layer. Proceedings of the 21st International Congress of Theoretical and Applied Mechanics, Warsaw, (2004)
  • [25] Lefebvre M.H., Fujiwara T.: Robust Euler Codes for Hypersonic Reactive Flows. Memories of the School of Engineering, Nagoya University, 46, No. 1, (1994)
  • [26] Mader C.L.: Numerical Modeling of Explosives and Propellants. Boca Raton, London, New York, Washoington D.C., (1988), CRC Press,.
  • [27] Sichel M., David T.S.: Transfer behind Detonations in H2-O2 Mixtures. AIAA Journal, 4, No. 6, (1966).
  • [28] Sichel M., Rao C.S. ,Nicholls J.A.: A simple theory of film detonation. Proceedings of Thirteenth Symposium on Combustion. The Combustion Institute, Pittsburgh, Pennsylvania, (1971).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BWM4-0028-0001
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