NEPE Propellant

High-energy aerospace propulsion

This propellant offers predictable burning rates and a significant enhancement when 1% HMX particles replace AP.

Kaixuan, Chen · Ye, Zhenwei · Xiao-Chun, Xue · Yu, Yonggang

Chemical Engineering Journal 2024

Specifications

of experimental data

{'zh': '10', 'en': '-2.5'} MPa

equation r b

{'zh': '', 'en': '3.93'} P

increases burning rate

{'zh': '1', 'en': '~0.02'} mm/s

Advantages

Adiabatic flame temperature 3200-3700 K