Propulsion Beal BA-2



BA-810 hot-fire

 

Stage

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp
kN N*s/kg kN N*s/kg tons s t/s MN*s
1

BA-4100

 11,980 2158 14,100 2540 721.7 130 5.5515 1,833.1
2

BA-810

     3,599 2765 214.7 165 1.3013 593.7
3

BA-44

     196.2 2942 40.0 600 0.0667 117.7