Feasibility Study and Demonstration of an Aluminum and Ice Solid Propellant

Table 3

Modeling summary for 5^′′ long grain.

Model assumptions	Total impulse (N-s)	Peak 𝑃𝑐 (MPa)	Peak thrust (kN)
No losses for 5^′′ long grain	1484	14.68	1.98
With deposit and losses for 5^′′ long grain	1336	14.82	1.78