Performance of Fuel-Rich Propellants for Ramjet Applications.

  • V.K. Bhat High Energy Materials Research Laboratory. Pune.
  • R.H. Brahmbhatt High Energy Materials Research Laboratory. Pune.
  • P.G. Shrotri High Energy Materials Research Laboratory. Pune.
  • Haridwar Singh High Energy Materials Research Laboratory. Pune.
DOI: https://doi.org/10.14429/dsj.46.4300
Keywords: Fuel-Rich Propellants, Hydroxy terminated, polybutadiene, zirconium, metal fue,

Abstract

A hydroxy terminated block copolymer-based fuel-rich propellant has been studied for gun and missile applications. The copolymer has shown certain advantages over hydroxy terminated polybutadiene. Zirconium was found as a promising metal fuel.

Author Biographies

V.K. Bhat, High Energy Materials Research Laboratory. Pune.
High Energy Materials Research Laboratory. Pune.
R.H. Brahmbhatt, High Energy Materials Research Laboratory. Pune.
High Energy Materials Research Laboratory. Pune.
P.G. Shrotri, High Energy Materials Research Laboratory. Pune.
High Energy Materials Research Laboratory. Pune..
Haridwar Singh, High Energy Materials Research Laboratory. Pune.
High Energy Materials Research Laboratory. Pune.
Published
2013-01-01
How to Cite
Bhat, V., Brahmbhatt, R., Shrotri, P., & Singh, H. (2013). Performance of Fuel-Rich Propellants for Ramjet Applications. Defence Science Journal, 46(5), 331-336. https://doi.org/10.14429/dsj.46.4300
Issue
Vol 46 No 5: High Energy Materials
Section
Special Issue Papers
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