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Original Articles

Rocket Propellant Combustion Studies in a Constant Volume Bomb

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Pages 149-157 | Received 26 Jul 1974, Published online: 21 May 2007

REFERENCES

  • Dhameja , R.K. , 1973 , Development of processing techniques and burning rate studies of composite propellants , M. E. Project Report , Department of Aeronautical Engineering, Indian Institue of Science , Bangalore .
  • Every , R. L. and Thieme , J. O. , 1965 , Liquid oxygen and liquid methane mixtures as rocket monopropellant . J. Spacecrafts and Rockets , 2 , 787 .
  • Fayon , A. M. and Goldstein , J. B. , 1966 , Evaluation of solid propellant ballistic properties by constant volume burning . Combustion and Flame , 10 , 23 .
  • Griffin , D. N. , Turner , C. F. , and Campbell , G. T. , 1959 , A ballistic bomb method for determining the experimental performance of rocket propellants . ARS Journal , 29 , 15 .
  • Twama , A. , Aoyagi , S. , Sofue , T. , and Yamazaki , K. , 1967 , Evaluation of ballistic performance of solid propellants by means of a constant volume bomb , ISAS Report No. 410 , University of Tokyo , 32 , 51 .
  • Mukunda , H. S. and Raghunandan , B. N. , 1974 , Some investigations on a constant volume bomb , Report No. AE C & P-3 , Department of Aeronautical Engineering, Indian Institute of Science , Bangalore .

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