Ammonium Nitrate Catalyzed with Copper Chromite Nanoparticles: A Novel Halogen Free Oxidizer for a Solid Propellant with Low Smoke Signature

Ammonium perchlorate (AP), the main oxidizer for solid propellants, results in white smoke (HCl); which could induce acidic rain and could damage fertile soil.A chlorine-free oxidizer is highly valued for solid propellants.Ammonium nitrate (AN) emerges as a promising green oxidizer; however it exhibits low performance (i.e.specific impulse).The present work describes the synthesis of copper chromite nanoparticles (NPs) of 45 nm.Copper chromite NPs were synthesized through hydrothermal synthesis; the developed nanocatalyst was then integrated into an AN matrix.While virgin AN demonstrated a strong endothermic decomposition of +1707 J/g, catalyzed AN demonstrated a superior exothermic decomposition, with an enthalpy of -1492 J/g.A solid propellant formulation based on AN and copper chromite (CuCr2O4) was optimized using the Institute for Chemical Technology (ICT) thermodynamic code via partial replacement of AP with AN.AN (30 wt.%) was found to decrease the smoke signature by 54.4%, with a minimum decrease in specific impulse.The solid propellant formulation was developed via mixing and vacuum casting.The ballistic performance was assessed using a small-scale ballistic evaluation rocket motor.The AN-based formulation demonstrated a stable combustion process with a slight decrease in the characteristic exhaust velocity and total pressure impulse of 4% and

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Publication Details

Journal
Central European Journal of Energetic Materials
Published
2025-06-30
DOI
https://doi.org/10.22211/cejem/207453
Primary Topic
Rocket and propulsion systems research
Type
article
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article

Ammonium Nitrate Catalyzed with Copper Chromite Nanoparticles: A Novel Halogen Free Oxidizer for a Solid Propellant with Low Smoke Signature

Sherif Elbasuney, Mohamed W. Attwa, A. Ashraf, Ahmed Fahd et al.
Central European Journal of Energetic Materials
Rocket and propulsion systems research
article

Ammonium Nitrate Catalyzed with Copper Chromite Nanoparticles: A Novel Halogen Free Oxidizer for a Solid Propellant with Low Smoke Signature

Sherif Elbasuney, Mohamed W. Attwa, A. Ashraf, Ahmed Fahd, Ali A. Said, Hosam E. Mostaf
article en

Abstract

Ammonium perchlorate (AP), the main oxidizer for solid propellants, results in white smoke (HCl); which could induce acidic rain and could damage fertile soil.A chlorine-free oxidizer is highly valued for solid propellants.Ammonium nitrate (AN) emerges as a promising green oxidizer; however it exhibits low performance (i.e.specific impulse).The present work describes the synthesis of copper chromite nanoparticles (NPs) of 45 nm.Copper chromite NPs were synthesized through hydrothermal synthesis; the developed nanocatalyst was then integrated into an AN matrix.While virgin AN demonstrated a strong endothermic decomposition of +1707 J/g, catalyzed AN demonstrated a superior exothermic decomposition, with an enthalpy of -1492 J/g.A solid propellant formulation based on AN and copper chromite (CuCr2O4) was optimized using the Institute for Chemical Technology (ICT) thermodynamic code via partial replacement of AP with AN.AN (30 wt.%) was found to decrease the smoke signature by 54.4%, with a minimum decrease in specific impulse.The solid propellant formulation was developed via mixing and vacuum casting.The ballistic performance was assessed using a small-scale ballistic evaluation rocket motor.The AN-based formulation demonstrated a stable combustion process with a slight decrease in the characteristic exhaust velocity and total pressure impulse of 4% and

Central European Journal of Energetic MaterialsVol. 22(2)
Openalex Percentile: Top 80%
Rocket and propulsion systems research
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Ammonium Nitrate Catalyzed with Copper Chromite Nanoparticles: A Novel Halogen Free Oxidizer for a Solid Propellant with Low Smoke Signature — Sherif Elbasuney, Mohamed W. Attwa, et al. · Central European Journal of Energetic Materials (2025) | TGRS Research Map | TGRS