Kinetic and experimental study of Mn(III) acetylacetonate for green hypergolic ignition in HTP/Kerosene systems
• Mn(III)AA catalyzes green HTP/kerosene hypergolic ignition. • IDTs as low as 25 ms achieved; initial fuel temperature expands envelope. • Kinetic analysis reveals efficient catalysis (low E a ). • Pre-exponential factor shows diminishing returns with catalyst. • Catalyst strongly accelerates chemical ignition phase. The transition towards non-toxic, high-performance spacecraft propulsion has positioned highly concentrated hydrogen peroxide (HTP) and kerosene as a leading green propellant combination. However, achieving reliable hypergolic ignition in non-polar hydrocarbons remains a critical challenge due to significant physical mixing limitations and high chemical activation barriers. This study investigates the catalytic efficacy of Manganese(III) acetylacetonate (Mn(III)AA) dissolved in aviation-grade kerosene to enable rapid hypergolicity with 98% HTP. High-speed imaging and thermal diagnostics were employed to map the ignition delay time (IDT) across a range of catalyst loadings (0.5–10 wt%) and oxidizer-to-fuel ratios (4.5–7.5). The results demonstrate that Mn(III)AA is highly effective, achieving a minimum IDT of 25 ms at 50°C. Kinetic analysis revealed a significant reduction in apparent activation energy (9 to 14 kJ/mol), accelerating the chemical reaction rate until the system becomes limited by physical mixing processes. Notably, a non-linear performance trend was observed, where catalyst additions beyond 5 wt% yielded diminishing returns, suggesting a saturation threshold for practical engine design. These findings establish Mn(III)AA as a viable, high-efficiency additive for green bipropellant systems.
Authors
- Prakhar Jindal (ORCID: https://orcid.org/0000-0002-5341-7809)
- Jyoti Botchu
Institutions
- Delft University of Technology (NL)
Publication Details
- Journal
- Aerospace Science and Technology
- Published
- 2026-03-03
- DOI
- https://doi.org/10.1016/j.ast.2026.112056
- Primary Topic
- Rocket and propulsion systems research
- Type
- article
- Field-Weighted Citation Impact
- 0.00