Back
to the Purdue AAE Propulsion main page.
Back
to the Satellite Propulsion page.
Daimler-Benz
CHT0.5 Thruster
Engine statistics
Specification
Thrust
0.5N
Power (kW/HP)
0.55/0.75
Propellant
Hydrazine
Isp
2230 m/s
Chamber Pressure
22 bar
Weight
195 g
Length
113 mm
Nozzle Diameter
4.8 mm