Ridvan Rocket Remake rrr · solid-propellant grain lab

Mission requirements

Propellant

Grain geometry

Simulation mode

Nozzle

Thermochemistry (CEA lookup)

Requirements check

Cross-section burn progress t=0.00 s

Burn time— s
Peak Pc— MPa
Peak thrust— N
Total impulse— N·s
Initial Kn—
Propellant— g
Sliver— g
Isp— s

Grain burnback — Ab(y)

Grain burnback — Kn(y)

Chamber pressure Pc(t)

Thrust F(t)

Show me the equations