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X-ray and Visual Investigations on the Combustion Process of Curved, Low-gas, Pyrotechnic Paths Used in Self-destruction Assemblies of Missile Fusing Systems

Treść / Zawartość
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Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The validation of the consistency of combustion front propagation along confined, low-gas, curved, pyrotechnic paths pressed into the grooves of the disc bodies of artillery and rocket ammunition fusing systems, is of critical importance as it concerns the functional reliability and safe usage of such types of ammunition. To validate the above consistency, Real Time X-ray Radioscopy (RTR) was utilized for the recording of the combustion process of curved pyrotechnic paths comprising two delay time segments. To confirm the observations obtained by the RTR technique, visual (VIS) recording was utilized for the unconfined pyrotechnic path. Due to the RTR and VIS techniques, evolution of the combustion process was recorded as a combustion front travelling along the pyrotechnic path. The combustion front had a convex shape. Using the VIS technique, a conical, bright tail was also observed behind the combustion front. The mean velocity of the propagation of the combustion front along each delay segment of the confined pyrotechnic path was determined on the basis of the RTR recordings. Using the RTR and VIS techniques, it was possible to quasi-continuously detect and record the combustion front movement along the confined and unconfined pyrotechnic paths, respectively. The VIS observations confirmed the RTR recording of the convex shape of the combustion front. In addition, the VIS technique allowed us to record the bright, conical tail.
Rocznik
Strony
596--606
Opis fizyczny
Bibliogr. 24 poz., rys., tab.
Twórcy
  • Military Institute of Armament Technology, 7 Prym. St. Wyszyńskiego street, 05-220 Zielonka, Poland
  • Military Institute of Armament Technology, 7 Prym. St. Wyszyńskiego street, 05-220 Zielonka, Poland
autor
  • Military Institute of Armament Technology, 7 Prym. St. Wyszyńskiego street, 05-220 Zielonka, Poland
Bibliografia
  • [1] Encyclopedia of Explosives and Related Items. Vol. 4, (Fedoroff, B.T.; Sheffield, O.E., Eds.), Picatinny Arsenal, Dover, NJ, 1969, pp. D.857-858, D.860, D.862.
  • [2] Hathaway, G.M.; Hathaway, C.F. Fuse for Shells. Patent US 729932, 1903.
  • [3] King’s Norton Metal Co. and others, Improvements in Fuses for Shells and other Explosive Projectiles. Patent GB 5654, 1909.
  • [4] Rheinishe Metalwaaren-und Mashinen Fabrik, An Improved Percussion Fuse for Projectiles in Which, if Desired, the Explosion Can Be Delayed by a Certain Amount after Percussion. Patent GB 18890, 1912.
  • [5] Carr, M.F. An Improved Time Fuse for Projectiles. Patent GB 108429, 1917.
  • [6] Austin, H. Improvements in Time Fuses for Explosive Shells and Bombs.Patent GB 124806, 1919.
  • [7] Goss, J.H. Fuse for Projectiles. Patent US 1508450, 1924.
  • [8] Pantoflicek, B. Pyrotechnic Safety Device, i.e. Combustible One. (in Polish) Patent PL 6215, 1927.
  • [9] Vickers Co. Ltd. and Johnson, F.G.L. Improvements in or Relating to Time Fuses for Projectiles. Patent GB 282120, 1927.
  • [10] Curtis’s and Harvey Ltd. and Grimwood, A.J., Improvements in and Relating to Fuse Compositions and to Fuses for Shells. Patent GB 283741, 1928.
  • [11] Hale, G.C. Delay Powder. Patent US 1805214, 1931.
  • [12] Hale, G.C. Delay Powder. Patent US 1877127, 1932.
  • [13] Hercules Powder Company, Improvements in Fuses for Explosive Shells. Patent GB 384776, 1932.
  • [14] Imperial Chemical Industries Co. Ltd., Improvements in or Relating to Fuses and Like Combustion Train Elements. Patent GB 492438, 1938.
  • [15] Hale, G.C. Delay Powder. Patent US 2450892, 1948.
  • [16] Hale, G.C.; Hart, D. Delay Powder. Patent US 2478918, 1949.
  • [17] Nowak, K. Disc Shaped Pyrotechnic Delay Element. (in Polish) Patent PL 72424, 1975.
  • [18] Simmons, B.H.O. Pyrotechnic Delay Devices. Patent US 1434788, 1976.
  • [19] Kaczmarski, S.; Kuśnierz, T.; Zarzycki, B. Artillery Fuse with Adjustable Delay Element. (in Polish) Patent PL 144528, 1988.
  • [20] Shevchenko, A.M.; Serdjukova, V.N.; Syzrantzev, V.F. Safety-Actuating Mechanism for Warheads of Rocket Ammunition. (in Russian) Patent RU 2301960, 2007.
  • [21] Gao, Z.; Yuan, L.; Cheng, K.; Li, G.; Li, C. Fuse Powder Ring Device for Artificial Hail Preventing and Precipitation Increasing Projectile. Patent CN 105890472, 2016.
  • [22] Khurmatulina, R.I.; Minibaeva, D.G.; Smetanina, N.D.; Maltseva, T.G.; Petrova, V.A.; Golubev, V.S. Low-Gas Slow Burning Compound. (in Russian) Patent RU 2185355, 2002.
  • [23] Ardasheva, L.F.; Minibaeva, D.G.; Smetanina, N.D. Retarding Low-Gas Compositions. (in Russian) Patent RU 2256638, 2005.
  • [24] Okhrimenko, Eh.F.; Minibaeva, D.G.; Smetanina, N.D. Retarding Low-Gas Composition. (in Russian) Patent RU 2237646, 2004.
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa Nr 461252 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2020).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-5a6f44a1-995b-4b5a-b7e0-a54791749637
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