A New Erosive Burning Model of Solid Propellant Based on Heat Transfer Equilibrium at Propellant Surface

Table 1

Propellant parameters.

Propellant	Composition	(kg/m^2)	(K)
4525 [24]		1500	1667
5051 [24]		1500	1667
4869 [24]		1500	1667
5542 T [24]		1550	2065
5565 T [24]		1650	2575
5555 T [24]		1650	2575
Propellant A [26]		1620	1690
Propellant C [26]		1700	2550
Propellant 1 [27]		1700	3041