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Cool Propellants: flame temperatures and force constants....

Cool Propellants: flame temperatures and force constants. New calculations taking into account the formation of methane and ammonia

Hodge D.L., Huggins S.D.
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Report No. 34/R/
50. Explosives Research And Development Establishment. Ministry Of Supply. Waltham Abbey. Essex. 1951. – 30 p.Calculations of the flame temperatures and force constants of certain "cool" gun propellants have been carried out, taking into account the formation of methane and ammonia. It has been shown that for propellants F.527/155 and P.428/180 the 'true' flame temperatures are 2045°K. and 2050°K. compared with the 'nominal' values of 1942°K. and 1950°K. obtained by neglecting the formation of these gases. The 'true' force constants arc respectively 1493 and 1453 inch-tons/lb. compared with 1474 and 1436 inch-tons/lb. In the ease of the propellants P.527/156 and F.428/181 having a 'nominal' flame temperature of 1700°K. the true flame temperatures are 1905 and 1915°K. respectively and the corresponding force constants nearly 5 per cent, above those obtained by neglecting the formation of methane and ammonia. Conditions for the deposition of carbon do not exist for any of these propellants under conditions of maximum pressure but in the case of F.428/180 and F.428/181 conditions are such that carbon deposition could occur if equilibrium were attained at the moment of shot ejection.Contents:
Abstract.
Object of Investigation.
Introduction.
Calculation of Gas Composition and Adiabatic.
Flame Temperature of a Propellant.
Conditions at the Muzzle.
The Propellants under Investigation
Description of Work.
Discussion of Results.
Acknowledgments.
Bibliography.
Idioma:
english
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PDF, 3.81 MB
IPFS:
CID , CID Blake2b
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