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Shorter Communication

SOLID PROPELLANT BURNING RATE DURING A PRESSURE TRANSIENT

Pages 69-73 | Received 03 Jan 1972, Published online: 10 May 2007

REFERENCES

  • Krier , H. , Tien J. S. , Sirignano , W. and Summerfield , M. ( 1968 ). Nonsteady Burning Phenomena of Solid Propellants Theory and Experiment . AIAA Journal 6 , 278 .
  • Merkle , C. L. , Turk , S. L. and Summerfield , M. ( 1969 ). Extinguishment of Solid Propellants by Depressuriza- tion Effects of Propellant Parameters , AIAA Preprint 69 – 176 .
  • Parker , K. and Summerfield , M. ( 1966 ). The Ignition Transient in Solid Propellant Rocket Motors , Princeton University , Dept. of Aerospace and Mechanical Sciences Report No. 769. (See Appendix II.)
  • Paul , B. E. , Levine , R. L. and Fong , L. Y. ( 1964 ). A Ballistic Explanation of the Ignition Pressure Peak , presented at AIAA Solid Propellant Rocket Conference , Palo Alto , Cal ., AIAA Preprint 64–121 .
  • von Elbe , G. ( 1966 ). Solid Propellant Ignition and Response of Combustion to Pressure Transients , ALAA Preprint 66–668 .
  • von Elbe , G. and McHale , E. T. ( 1968 ). Extinguishment of Solid Propellants by Rapid Depressurization . AIAA J . 6 , 1417 ,

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