Performance of Fuel-Rich Propellants for Ramjet Applications.

Authors

  • 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.

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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

License

 Where otherwise noted, the Articles on this site are licensed under Creative Commons License: CC Attribution-Noncommercial-No Derivative Works 2.5 India

 

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