Application of transient burning rate model of solid propellant in electrothermal-chemical launch simulation

Ni, Yingchun; Jin, Yong; Wan, Gang; Yang, Chao; Li, Haiyuan; Li, Baoming

doi:10.1016/j.dt.2015.10.003

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Cited by 8 publications

(1 citation statement)

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“…A fundamental method used to propel rockets, bombs and missiles is the combustion of single and multi based propellants [1]. Solid propellants are commonly used for military purposes.…”

Section: Introductionmentioning

confidence: 99%

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Szala

Hara

Szymańczyk

et al. 2017

Propellants Explo Pyrotec

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Guanidinium and triaminoguanidinium azotetrazolate (GUAZ, TAGAZ) were used as high-nitrogen compounds for the preparation of new propellants bound with nitrocellulose and plasticized with dibutyl phthalate and 3methyl-3-nitroxymethyloxetane. The new propellant compositions were tested by using a differential thermal analy-sis-thermogravimetric technique, friction sensitivity and impact were ascertained and pyrostatic tests were conducted. Regardless of the amount of TAGAZ and plasticizer type, the propellants exhibit similar maximum pressure of the gases which allow for the replacement of NC in propellants by TAGAZ.

show abstract

“…A fundamental method used to propel rockets, bombs and missiles is the combustion of single and multi based propellants [1]. Solid propellants are commonly used for military purposes.…”

Section: Introductionmentioning

confidence: 99%

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Szala

Hara

Szymańczyk

et al. 2017

Propellants Explo Pyrotec

View full text Add to dashboard Cite

show abstract

Simulation of two-dimensional interior ballistics model of solid propellant electrothermal-chemical launch with discharge rod plasma generator

Jin

Cheng

et al. 2017

Defence Technology

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Numerical simulation on the pressure wave in a 30 mm electrothermal-chemical gun with the discharge rod plasma generator

Jin

Wan

et al. 2019

Defence Technology

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Application of transient burning rate model of solid propellant in electrothermal-chemical launch simulation

Cited by 8 publications

References 13 publications

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Simulation of two-dimensional interior ballistics model of solid propellant electrothermal-chemical launch with discharge rod plasma generator

Numerical simulation on the pressure wave in a 30 mm electrothermal-chemical gun with the discharge rod plasma generator

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Application of transient burning rate model of solid propellant in electrothermal-chemical launch simulation

Cited by 8 publications

References 13 publications

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Preliminary Study of New Propellants Containing Guanidinium or Triaminoguanidinium Azotetrazolate

Simulation of two-dimensional interior ballistics model of solid propellant electrothermal-chemical launch with discharge rod plasma generator

Numerical simulation on the pressure wave in a 30 mm electrothermal-chemical gun with the discharge rod plasma generator

Contact Info

Product

Resources

About

Numerical simulation on the pressure wave in a 30 mm electrothermal-chemical gun with the discharge rod plasma generator