Specification
- Two 400 lbf (1.8 kN) thrust rocket engines (non throttleable, restartable in flight)
- 20 sec 500 m takeoff roll
- Vne = 195 kt
- climb rate = 52 m/s (10,000 ft/min)
- maximum altitude = 10,000 ft
- Fuel : isopropyl alcohol and liquid oxygen
- Chamber pressure : ~ 350 psi
- specific impulse : 250 to 270 seconds
- Noise: 128 dB at 10 meters
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