PL EN


Preferencje help
Widoczny [Schowaj] Abstrakt
Liczba wyników
Tytuł artykułu

Studies on Aluminized, High Burning Rate, Butacene® Based, Composite Propellants

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
This paper reports on a Butacene® based composite propellant with high burning rate. The effect of replacing HTPB with Butacene® on the physical, mechanical and ballistic properties, and sensitivity towards impact and friction, has been studied. The ballistic properties were evaluated as burning rates at various pressures (7-11 MPa), pressure exponents, ignition temperatures etc. As expected, a remarkable enhancement in burning rate at low pressures was observed with increasing percentage of Butacene®. Comparatively lower n-values were observed for compositions containing Butacene® than for HTPB based propellants. The sensitivity of Butacene® based compositions, in terms of impact and friction, was found to be increased with an increasing percentage of Butacene®.
Słowa kluczowe
Rocznik
Strony
323--333
Opis fizyczny
Bibliogr. 16 poz., rys.
Twórcy
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
autor
  • High Energy Materials Research Laboratory, Sutarwadi, Pune-411021, India
Bibliografia
  • [1] Menke K., Boehnlein-Mauss J., Brehler K.P., Jungbluth H., Kalischewski W., New Ferrocenes for Burn-rate Modification of Composite Propellants, Proc. ADPA Int. Symp. on Energetic Materials Technology, Phoenix, Arizona, US, Sept. 24-27, 1995.
  • [2] Boehnlein-Mauss J. Bohn M.A., Menke K., Gottlieb K., Junqbluth H., Lohmann G., Thunker W., Brehler K.P., Structural Influences of Ferrocenes on Burn Rate Modification of Composite Rocket Propellants, 24th Int. Annu. Conf. ICT, Karlsruhe, Germany, 1993, pp. 71/1-71/19.
  • [3] Hong M.P., Lee B.J., Ferrocene Dicarboxylic Acid Diesters and Solid Composite Propellant Containing the Same, Pollimo, 1997, 21(2), 302-308.
  • [4] Mackowiak H., Gottlieb K., Ferrocene Dicarboxylic Acid Diesters and Solid Composite Propellants Containing the Compounds, PCT Int. Appl. WO 9850396, 1998.
  • [5] Gore G.M., Tipre K.R., Bhatewara R.G., Prasad U.S., Gupta M., Mane S.R, Evaluation of Ferrocene Derivatives as Burn Rate Modifiers in AP/HTPB Based Composite Propellants, Def. Sci. J., 1999, 49(2), 151-158.
  • [6] Raynal S., Doriath G., Proc., 22nd Joint Propulsion Conference, AIAA-86-1594,Alabama, 1986.
  • [7] Gotzmer C., Cziesla M.J., Non-migrating Ferrocene Containing Solid Propellant Binder, US Patent 4,168,362,1979.
  • [8] Nguyen T.T., The Effects of Ferrocenic and Carborane Derivative Burn Rate Catalysts in AP Composite Propellant Combustion Mechanism of Ferrocenecatalysed Combustion, DSTO-TR-0121, 1995.
  • [9] Gore G.M., Nazare A.N., Divekar C.N., Hait S.K., Asthana S.N., Studies on Nonaluminized High Burning Rate AP-composite Propellants, J. Energ. Mater., 2004, 22, 151-169.
  • [10] Christiansen W.N., Development of an Acoustic Emission Strand Burning Technique for Burning Rate Prediction, AIAA/SAE, 14th Joint Propulsion Conference, Las Vegas, 1978, 25-27.
  • [11] Rinford J.H., Technical Review to Advanced Techniques in Acoustical, Electrical and Mechanical Measurements, Bruel and Kjaer, DK-2850 NAERUM, Denmark, 1981, vol. 2, p. 3.
  • [12] Mallory D.H., Development of ImpactSensitivity Test at Explosive Research Laboratory, Bruceton Pennsylvania, NAVORD, Report No. 4236, 1960.
  • [13] Peters J.K.G., Proc. of the Production Program of Julius Peter Company for Members of M.B.B., Course-81, Berlin, 1921, p. 14.
  • [14] Doriath G., Energetic Insensitive Propellants for Solid and Ducted Rockets, J. Propul. Power, 1995, 11(4), 870-882.
  • [15] Doriath G., High Burning Rate Solid Rocket Propellants, Int. J. Energ. Mater. Chem. Propul., 1997, 4, 646-660.
  • [16] Kishor K., Shridhara K., Solid Propellant Chemistry, Defence Research and Development Organization, Ministry of Defence, New Delhi, India, 1999, p. 117.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-a82ffcb0-bafd-4087-8b2c-221bf811e5d8
JavaScript jest wyłączony w Twojej przeglądarce internetowej. Włącz go, a następnie odśwież stronę, aby móc w pełni z niej korzystać.