Engines Black Arrow


Solid RPE Waxwing

  
Twin-chamber engine "Stentor" for air-to-air missile Blue Steel (107 + 27 kN)



Gamma 8 (eight small Stentor chambers)


 
Engine Gamma 2 (two small Stentor chambers with nozzle extension)

 

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 Gamma 8 (8) 224.4 2461 234.8 2599 13.034 144.2 0.0904 33.9
2 Gamma 2 (2)     68.2 2569 3.002 113 0.0266 7.7
3 RPE Waxwing     29.4 2726 0.303 28 0.0108 0.8