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- [3] Thermal decomposition characteristics of aluminum-magnesium fuel-rich propellant Tuijin Jishu/Journal of Propulsion Technology, 2000, 21 (05): : 77 - 80
- [4] Flammability limits of aluminum-magnesium fuel-rich propellant Tuijin Jishu/Journal of Propulsion Technology, 1999, 20 (02): : 95 - 98
- [5] Combustion characteristics of boron-based fuel-rich propellant at low pressure Hu, S.-Q., 1600, Journal of Propulsion Technology (23): : 518 - 520
- [6] Theoretical analysis on combustion residue of magnesium-aluminum fuel-rich propellant Guti Houjian Jishu, 2006, 3 (200-203):
- [7] Aluminum, magnesium content determination in fuel-rich propellant by potentiometric titration ISTM/2005: 6th International Symposium on Test and Measurement, Vols 1-9, Conference Proceedings, 2005, : 2745 - 2747
- [8] Effect on primary combustion performance of aluminum particle size in fuel-rich propellant with high aluminum content Guti Huojian Jishu/Journal of Solid Rocket Technology, 2010, 33 (06): : 670 - 674
- [10] Progress in combustion characteristics of boron-based fuel-rich propellant Hanneng Cailiao, 2007, 4 (436-440):