Prediction of Advanced Nitramine Propellant Burning Rates with the CYCLOPS Code

Miller, Martin S.; Anderson, William R.

doi:10.21236/ada416019

Cited by 4 publications

(4 citation statements)

References 9 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

Section: Resultsmentioning

confidence: 97%

“…The scatter of the literature data may be a consequence of differences in the characteristics of JA-2 produced by various producers. As stated in the report [23], the burning rates of JA-2 produced in Germany and in the US may differ by 20%. The scatter of the literature data may be a consequence of differences in the characteristics of JA-2 produced by various producers.…”

Section: Resultsmentioning

confidence: 97%

“…The scatter of the literature data may be a consequence of differences in the characteristics of JA-2 produced by various producers. As stated in the report [23], the burning rates of JA-2 produced in Germany and in the US may differ by 20%. LO5460 propellant is a good example of coarse-grained propellants with regular shapes of grains.…”

Section: Resultsmentioning

confidence: 97%

See 2 more Smart Citations

Determining the Burning Rate of Fine-Grained Propellants in Closed Vessel Tests

2022

View full text Add to dashboard Cite

This paper presents the method of determining the burning rate of fine-grained propellants based on the results of closed vessel tests. It is shown that in the case of fine-grained propellants, the standard methods of determining the burning rate fail. There are two reasons for this: imperfections of the grain shapes and the prolonged process of ignition due to a more developed surface than that of coarse grains at the same mass of the propellant. The value of the exponent in the burning law is estimated by the use of the so-called experimental form–function. The upper and lower limits of the value of the coefficient in the burning law are estimated. The accuracy of the proposed method is analyzed. Its validity is assessed by comparing the results of closed vessel tests analysis with accessible literature data.

show abstract

Section: Resultsmentioning

confidence: 97%

Section: Resultsmentioning

confidence: 97%

See 1 more Smart Citation

Determining the Burning Rate of Fine-Grained Propellants in Closed Vessel Tests

2022

View full text Add to dashboard Cite

show abstract

“…Densities (117) for RDX and BAMO are 1.816 and 1.30 g/cm 3 , respectively, from which we estimate the propellant density as 1.7 g/cm 3 . L DZ and r b were 0.27 ± 0.07 cm and 0.14 cm/s, respectively.…”

Section: Litzinger Et Al Rdx/bamo Propellantmentioning

confidence: 85%

Dark Zones of Solid Propellant Flames: Critical Assessment and Quantitative Modeling of Experimental Datasets With Analysis of Chemical Pathways and Sensitivities

Anderson¹,

Meagher²,

Vanderhoff³

2011

Self Cite

View full text Add to dashboard Cite

Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing the burden, to Department of Defense, Washington Headquarters Services, Directorate for Information Operations and Reports (0704-0188), 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302. Respondents should be aware that notwithstanding any other provision of law, no person shall be subject to any penalty for failing to comply with a collection of information if it does not display a currently valid OMB control number. 16. SECURITY CLASSIFICATION OF: 17. LIMITATION OF ABSTRACT UU 18. NUMBER OF PAGES 202 19a. NAME OF RESPONSIBLE PERSON

show abstract

Shock tube study of the pressure dependence of monomethylhydrazine pyrolysis

Davidson

Hanson

2014

Combustion and Flame

View full text Add to dashboard Cite

Prediction of Advanced Nitramine Propellant Burning Rates with the CYCLOPS Code

Cited by 4 publications

References 9 publications

Determining the Burning Rate of Fine-Grained Propellants in Closed Vessel Tests

Determining the Burning Rate of Fine-Grained Propellants in Closed Vessel Tests

Dark Zones of Solid Propellant Flames: Critical Assessment and Quantitative Modeling of Experimental Datasets With Analysis of Chemical Pathways and Sensitivities

Shock tube study of the pressure dependence of monomethylhydrazine pyrolysis

Contact Info

Product

Resources

About