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Volumn 56, Issue 4, 2006, Pages 543-550

Combustion characteristics of coated nano aluminum in composite propellants

Author keywords

Aluminium powder; Combustion; Composite propellants; Micron sized aluminium powder; Nano sized aluminium powder; Nanostructured materials; Nanotechnology

Indexed keywords

ALUMINUM POWDER METALLURGY; IGNITION; NANOSTRUCTURED MATERIALS; NANOTECHNOLOGY; SCANNING ELECTRON MICROSCOPY; X RAY ANALYSIS;

EID: 33751027964     PISSN: 0011748X     EISSN: None     Source Type: Journal    
DOI: 10.14429/dsj.56.1919     Document Type: Article
Times cited : (8)

References (11)
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  • 3
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    • edited by K.K. Kuo, et al. Begell House
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    • (1997) Challenges in Propellants and Combustion 100 Years after Nobel , pp. 636-645
    • Ivanov, G.V.1    Tepper, F.2
  • 6
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    • Propellant burning rate enhancement and thermal behavior of ultra-fine aluminum powder (ALEX)
    • ICT held at Karisruhe, Germany, 30 June-3 July
    • Mench, M.M.; Yeh, C.L. & Kuo, K.K. Propellant burning rate enhancement and thermal behavior of ultra-fine aluminum powder (ALEX). In 29th International Annual Conference on Energetic Materials, ICT held at Karisruhe, Germany, 30 June-3 July, 1998. pp. 30/1-15
    • (1998) 29th International Annual Conference on Energetic Materials
    • Mench, M.M.1    Yeh, C.L.2    Kuo, K.K.3
  • 7
    • 7244247271 scopus 로고    scopus 로고
    • Effect of nano aluminum and nickel powders on the combustion properties of composite propellant
    • Zhi, J. & Li, S.F. Effect of nano aluminum and nickel powders on the combustion properties of composite propellant. J. Propu. Tech., 2004, 25(4), 368-73.
    • (2004) J. Propu. Tech. , vol.25 , Issue.4 , pp. 368-373
    • Zhi, J.1    Li, S.F.2
  • 8
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    • Temperature sensitivity of the burning rate of composite solid propellants
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    • Cohen-Nir, E.1
  • 9
    • 33751037950 scopus 로고    scopus 로고
    • Influence of aluminum radiative heat feedback on pressure exponent
    • Zhu, J.; Li, S.F. Influence of aluminum radiative heat feedback on pressure exponent. J. Solid Rocket Technol., 1998, 21(1), 31-34.
    • (1998) J. Solid Rocket Technol. , vol.21 , Issue.1 , pp. 31-34
    • Zhu, J.1    Li, S.F.2
  • 11
    • 0032188394 scopus 로고    scopus 로고
    • Effect of fuelbinder and oxidiser particle diameter on combustion ammonium perchlorate-based propellants
    • Al-Harthi, A. & Williams, A. Effect of fuelbinder and oxidiser particle diameter on combustion ammonium perchlorate-based propellants. Fuel, 1998, 77(13), 1451-68
    • (1998) Fuel , vol.77 , Issue.13 , pp. 1451-1468
    • Al-Harthi, A.1    Williams, A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.