Project

Engine

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

Falcon-X

Merlin -2 (1)

7,562

2795

8,540

3157

2.7055

Eagle

Griffon -1A (1)

5,338

2648

5,910

2877

2.0540