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Factors Affecting the Measurement of the Percentage of Gaseous Products from Boron-based Fuel-rich Propellants

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
Acid-washed asbestos, carbon fibre, and MgO with carbon fibre were used as the filter media in order to compare their filtering qualities in the estimation of the percentage of gaseous products (PGP) arising from the combustion of singlebase propellants, double-base propellants, and boron-based fuel-rich propellants. The comparison was based on an analysis of the experimentally registered influence of the propellant formulation, the propellant load, the maximum chamber pressure and the thickness of the MgO filter layer on the PGP from the fuel-rich propellant, and in particular on the PGP produced by combustion of boron-based fuel-rich propellant. The results showed that the experimental values of the PGP were closer to the theoretically predicted values when carbon fibre mixed with MgO powder was used as the filter medium. The PGP of boron-based fuel-rich propellant increased when the AP was in part replaced by HMX, when the AP content was increased and when boron was in part replaced by magnesium-aluminum alloy. In terms of the apparatus used in these experiments, the propellant loading density was found to have little correspondence with the PGP for boron-based fuel-rich propellant. The optimal propellant loading density for the chamber volume of 85 cm3 was found to be 2-2.5 g, in view of the reliability and safety of the experiment. It is emphasised that the thickness of the MgO filter layer is very important for the accuracy and reliability of the experiment, and that the optimum should be determined by experiment.
Rocznik
Strony
15--29
Opis fizyczny
Bibliogr. 15 poz., rys., tab.
Twórcy
autor
  • Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
autor
  • Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
autor
  • Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
autor
  • Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072, China
Bibliografia
  • [1] Besser H.L., Overview of Boron Ducted Rocket Development During the Last Two Decades , (Kuo K.K., Pein R., Eds.), Begell House and CRC Press, 1993.
  • [2] Wei Zhang, Hui Zhu, Combustion Property of Aluminum-Magnesium Fuel-rich Propellant at Low Pressure, 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference , Huntsville, Alabama, July 17-19, 2000 .
  • [3] Chen D.M., Luh S.P., Liu T.K., Combustion Study of Boron-based Fuel-rich Solid Propellant , (K.K. Kuo, R. Pein, Eds.), Begell House and CRC Press, 1993.
  • [4] Gany A., Timnat Y.M., Advantages and Drawbacks of Boron-fueled Propulsion, Acta Astronaut. , 1993, 29 (3), 181-187.
  • [5] Gany A., Comprehensive Consideration of Boron Combustion in Airbreathing Propulsion, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, California, 2006.
  • [6] Bao F.T., Huang J.X., Integral Solid Propellant Ramjet Rocket Motor (in Chinese), Beijing, China Astronautic Publishing House, 2006.
  • [7] Miyayama T., Oshima H., Improving Combustion of Boron Particles in Secondary Combustor of Ducted Rockets, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, California, 2006.
  • [8] Liu L.L, He G.Q., Study on the Calculation of the Combustion Products of the Boron-based Fuel-rich Propellant During the First Combustion Stage (in Chinese), Chin. J. Explos. Propellants , 2013 , 36 (2), 46-51.
  • [9] Wang Y.H., Chen Ch., Investigation on Measuring Gas Generation Rate for Fuel-rich Propellant During Combustion Process (in Chinese), J. Solid Rocket Technol., 2009 , 32 (5), 588-590.
  • [10] Purchas D.B., Sutherland K., Handbook of Filter Media (2nd ed.), Elsevier Science Inc., New York, 2002
  • [11] Corn M., Handbook of Hazardous Materials , Academic Press Inc., London, 1993.
  • [12] Chung D.D.L., Carbon Fiber Composites , Butterworth-Heinemann, Massachusetts, 1994.
  • [13] Sanford G., McBride B.J., Computer Program for Calculation of Complex Chemical Equilibrium Composition and Applications, I. Analysis , NASA Reference Publication, 1994 .
  • [14] McBride B.J., Sanford G., Computer Program for Calculation of Complex Chemical Equilibrium Compositions and Applications, II. Users Manual and Program Description , NASA Reference Publication, 1996 .
  • [15] Kuo K.K., Summerfield M., Fundamentals of Solid-propellant Combustion, American Institute of Aeronautics and Astronautics, 1984.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-bbc39130-27c4-4ec3-9573-d79619f1bb6f
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