2017
DOI: 10.1088/1742-6596/909/1/012077
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Stabilizer Effect on Thermal Decomposition of Aged Solid Propellant

Abstract: Abstract. Composite solid propellants experience aging process during storage, and their properties will alter. The stabilizer added was used to reduce the effects of aging. This research studied the influence of the stabilizer on changes of the composite solid propellant thermal decomposition due to the onset of aging during the 40 days of storage at a temperature of 333 K. AO 2246 as a stabilizer added by as much as 0 to 1% by weight of propellant binders. The testing method used is heating the samples at va… Show more

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Cited by 4 publications
(3 citation statements)
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“…With the wide application of solid rocket motors in missile weapons and various strategic launch vehicles, people have begun to study their storage performance extensively [2][3]. Solid propellants will age during storage [4][5][6][7] and storage aging performance is one of the essential properties of solid propellants [8]. In-depth research on solid propellant aging performance is important for guiding the long-term storage safety of propellants [9][10].…”
Section: Introductionmentioning
confidence: 99%
“…With the wide application of solid rocket motors in missile weapons and various strategic launch vehicles, people have begun to study their storage performance extensively [2][3]. Solid propellants will age during storage [4][5][6][7] and storage aging performance is one of the essential properties of solid propellants [8]. In-depth research on solid propellant aging performance is important for guiding the long-term storage safety of propellants [9][10].…”
Section: Introductionmentioning
confidence: 99%
“…The presence of decomposition products (RÀ O, NO x ) and acid (HNO 3 ) speed up the degradation by attacking the yet undecomposed nitrate esters from NC in the propellant matrix [6]. Calorimetric tests revealed a loss of energy and an increase in temperature of the propellant, which has the effect of minimising its efficiency and reducing its lifetime [7][8][9][10][11][12]. To solve this issue, stabilisers are added to propellants.…”
Section: Introductionmentioning
confidence: 99%
“…A succession of secondary reactions like acid-base reactions, hydrogen abstractions and oxidations occur and produce gases such as CO, and especially NO and NO 2 [2,4]. These reactions have been studied using calorimetric tests which have revealed a loss of energy and an increase in temperature of the powder, which influences the performance of the propellant and reduces its lifetime [5][6][7][8][9][10].…”
Section: Introductionmentioning
confidence: 99%