Table 1. Calculated Parameters of Basic Properties of Different Propellants^a.

component			properties
NC/%	NG/%	additives (10%)	OB/%	M/(mole·kg–1)	f/(kJ·kg–1)	Tv/K
100			–31.84	39.55	1065.09	3238.83
90		TEGDN	–35.32	40.98	1054.89	3095.90
90		PNA	–48.63	44.63	903.95	2436.12
90		DBP	–51.07	44.95	903.93	2418.41
90	10		–28.30	38.74	1101.43	3419.29
81	9	TEGDN	–32.13	40.24	1091.25	3261.81
81	9	PNA	–45.45	43.97	952.27	2604.92
81	9	DBP	–47.89	44.34	953.20	2585.80

^aOB, oxygen balance.

^bM, total molar number of generated gases.

^cf, force.

^dT_v, flame temperature.

^eNitrogen content of NC, 13%.