Abstract This paper investigates the effects of different boron-based combustion modifiers on the rheological, combustion and energy release characteristics of boron-based fuel-rich propellants. The results show that boron-based high-energy ionic salts (B1, B2, B3) and boron-based metallic fuels (Mg-Al-B), when combined with (AB+TAB)/HTPB mixed systems, exhibit superior rheological characteristics. The B2 and Mg-Al-B agglomerated particles demonstrate low apparent activation energy and high reaction rate constants, facilitating the rapid combustion of boron-based fuel-rich propellants. Furthermore, the synergistic catalytic effect of B2 and Mg-Al-B increases the static burning rate pressure index from 0.38 to 0.54 at 0.5∼5 MPa, with a dynamic pressure index of 0.52. These modifications improve the energy release efficiency η c1 of the propellant, the energy release efficiency η c2 of the primary combustion, and the combustion efficiency η B of boron powder by 12.93%, 24.61%, and 34.06%, respectively. The primary injection efficiency exceeds 98%, significantly enhancing the combustion performance and energy release efficiency of boron-rich fuels.
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