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
Authors
- Sherif Elbasuney (ORCID: https://orcid.org/0000-0002-6973-3830)
- Mohamed W. Attwa (ORCID: https://orcid.org/0000-0002-1147-4960)
- A. Ashraf (ORCID: https://orcid.org/0009-0000-9003-6928)
- Ahmed Fahd
- Ali A. Said
- Hosam E. Mostaf
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
- Field-Weighted Citation Impact
- 0.00