Propulsion Astra Rocket
 



Electric pump engine "Delphin" (RP-1/LOX)


 



Pressure-fed engine "Aether" (RP-1/LOX)

 

Rocket 3.1

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 t sec t/s MN*sec
1 Delphin (5) 140.1 ? ? ?  ? 138    
2 Aether     3.0 ?  ? 376    

 

Rocket 3.3

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 t sec t/s MN*sec
1 Delphin (5) 144.6 ? ? ? ? 170    
2 Aether     3.3 ?  ? 325    

 



Firefly Reaver engine (two combustors)



Ursa Major Hadley vac engine

 

Rocket 4.0

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 t sec t/s MN*sec
1 Reaver (2) 333.7 2899 368.0 3197 ?   0.1151  
2 Hadley vac     27.1 3614 ?   0-0075