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Titolo:
SPECIFIC-HEATS OF SOLID GUN PROPELLANTS
Autore:
MILLER MS;
Indirizzi:
USA,RES LAB ABERDEEN PROVING GROUND MD 21005
Titolo Testata:
Combustion science and technology
fascicolo: 1-6, volume: 102, anno: 1994,
pagine: 273 - 281
SICI:
0010-2202(1994)102:1-6<273:SOSGP>2.0.ZU;2-Z
Fonte:
ISI
Lingua:
ENG
Keywords:
SPECIFIC HEAT; SOLID PROPELLANT; GUN PROPELLANT;
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Science Citation Index Expanded
Science Citation Index Expanded
Science Citation Index Expanded
Citazioni:
6
Recensione:
Indirizzi per estratti:
Citazione:
M.S. Miller, "SPECIFIC-HEATS OF SOLID GUN PROPELLANTS", Combustion science and technology, 102(1-6), 1994, pp. 273-281

Abstract

Measurements are reported of the specific heat of 5 U.S. Army solid gun propellants over the temperature range - 40 degrees C to 75 degreesC at atmospheric pressure. The propellants are members of the BRL Research Series propellants that have been widely distributed to researchlaboratories in the U.S. These propellants include representative types from each class of materials that are either in the fielded inventory or experimental (''X'' prefix), i.e., a single base (M10), a doublebase (M9), a homogeneous triple base (JA2), a composite triple base (M30), and a composite nitramine (XM39). The measurements were performed with a commercial differential scanning calorimeter (DSC) which was calibrated to the propellant heat-flow range using two sapphire standards of different masses. Corrections were made for temperature lags inboth the standard and propellant specimens. The average values are estimated to be accurate to within +/- 5%, and polynomial fits over the stated temperature range are provided for convenient use in calculations.

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Documento generato il 23/09/20 alle ore 22:13:35