Propulsion LauncherOne


 
Newton-3 ......



........ without nozzle


Newton-3


Newton-4 ?

Old concept

Stage

Engine

Type

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Isp
kN N*s/kg kN N*s/kg t sec t/s MN*sec
1

Newton-2

Gas Gen.     211.3          
2

Newton-1

Pressure fed     15.6 2942     0.0053  

 

Stage

Engine

Type

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Isp
kN N*s/kg kN N*s/kg t sec t/s MN*sec
1 Newton-3 Gas Gen. (2)     326.9 ~2942 ~20.0 180 0.1111 58.8
2 Newton-4 Gas Gen.     22.2 ~2042 ~2.75 360 0.0076 8.1