Abstract:a]
1I ntroductionAmmonium perchlorate (AP) composite propellants are widely used in solid rocket propulsion. Common formulations for AP composite propellants include hydroxyl-terminated polybutadiene (HTPB) as ab inder and fuel, ac urative/plasticizer to solidify the HTPB binder,s ometimes aluminum particles as fuel to increase energy density,a nd sometimes am etal oxide additive to catalyze AP thermal decomposition [1].T he burning rate of AP composite propellants has been shown to be controlled by the concen… Show more
“…The doping of AP with transition metals and their oxides has shown to decrease the activation energy and decomposition temperature of AP, thereby acting as good catalysts (Schumacher, 1960;Boldyrev, 2006;Jacobs & Whitehead, 1969;Kishore & Sunitha, 1979). The mechanical mixing of AP with compounds of copper and iron is highly effective in reducing the thermal decomposition of Ammonium perchlorate (Wang et al, 2013;Patil, Krishnamurthy & Joshi, 2008;Chen, Li & Li, 2008b, 2008aAlizadeh-Gheshlaghi et al, 2012;Yang et al, 2014;Liu et al, 2004;Chaturvedi & Dave, 2013;Styborski et al, 2015;Song et al, 2010;Costa et al, 2009).…”
Ammonium perchlorate (AP) is the universal oxidiser in use for all the solid rocket propellant motors used for space exploration due to its high available oxygen content and thermal decomposition without any solid residue. The inclusion of reactive species in AP directly affect the viscoelastic and ballistic properties of the propellant. Variations in lattice configuration of AP change its physical and thermal characteristics dramatically. In the present work AP was doped with Copper perchlorate and Iron perchlorate through co crystallisation. The impact of inclusion of these ionic species in the lattice on the thermal decomposition characteristics of AP was examined. The incorporation affected the physical as well as the ballistic characteristics of the resultant AP. The incorporation of foreign ions into AP crystals significantly changed the crystal morphology. The decomposition temperature decreased vis-a-vis with normal AP. The activation energy remarkably decreased for the doped AP crystals.
“…The doping of AP with transition metals and their oxides has shown to decrease the activation energy and decomposition temperature of AP, thereby acting as good catalysts (Schumacher, 1960;Boldyrev, 2006;Jacobs & Whitehead, 1969;Kishore & Sunitha, 1979). The mechanical mixing of AP with compounds of copper and iron is highly effective in reducing the thermal decomposition of Ammonium perchlorate (Wang et al, 2013;Patil, Krishnamurthy & Joshi, 2008;Chen, Li & Li, 2008b, 2008aAlizadeh-Gheshlaghi et al, 2012;Yang et al, 2014;Liu et al, 2004;Chaturvedi & Dave, 2013;Styborski et al, 2015;Song et al, 2010;Costa et al, 2009).…”
Ammonium perchlorate (AP) is the universal oxidiser in use for all the solid rocket propellant motors used for space exploration due to its high available oxygen content and thermal decomposition without any solid residue. The inclusion of reactive species in AP directly affect the viscoelastic and ballistic properties of the propellant. Variations in lattice configuration of AP change its physical and thermal characteristics dramatically. In the present work AP was doped with Copper perchlorate and Iron perchlorate through co crystallisation. The impact of inclusion of these ionic species in the lattice on the thermal decomposition characteristics of AP was examined. The incorporation affected the physical as well as the ballistic characteristics of the resultant AP. The incorporation of foreign ions into AP crystals significantly changed the crystal morphology. The decomposition temperature decreased vis-a-vis with normal AP. The activation energy remarkably decreased for the doped AP crystals.
“…13 To achieve this target, numerous researches have been studied based on adding some additives such as metals or nitramines (RDX, HMX, etc.). [14][15][16][17][18] Several groups worldwide have intensively investigated other compounds to substitute AP to overcome its toxicity problems and to enhance the energetic characteristics, sensitivities and thermal properties. [19][20][21] These compounds are based on orthocarbonates, tetrazoles, carbamates, nitrocarbamates, formates, pyrazoles and triazoles.…”
“…There are several ways of improving the parameters of such propellants. It is possible to use burning rate modifiers (catocene, butacene, nano-Fe 2 O 3 ) [6][7][8][9], or to apply highly energetic binder compounds like NHTPB, BAMO, GAP etc. [10][11][12].…”
This paper presents results from the application of [Cu(TNBI) (NH3)2(H2O)] (CuTNO) to heterogeneous solid rocket propellants based on HTPB/AP, replacing RDX. A series of different compositions of solid heterogeneous rocket propellants based on HTPB and ammonium perchlorate, containing CuTNO or RDX, were prepared and investigated. The ballistic parameters of the examined propellants were determined by combustion in a laboratory rocket motor (LRM). The ballistic properties were evaluated in the pressure range 4-10 MPa and it was found that the linear burning rate at 10 MPa increased by more than 20% for the CuTNO containing propellant, compared to the RDX-based composition. By linear regression of the r = f(p) curves obtained, the burning laws for the investigated propellants were determined. It was found that the CuTNO additive increases the pressure coefficient by over 46%, compared to unmodified propellant. The determination of the sensitivities to friction and impact, the calorific value, hardness and decomposition temperature of the propellants obtained were also investigated.
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