Propellants, Fuel/Oxidizer …..НДМГ/АТИН, AT
Mixture Ratio …..1,85±0.15
Average Nominal Thrust, N (Ibf) ….... 490
Average Specific Impulse, Steady State, sec….. 315
Nominal Inlet Pressure, MPa (psi) ….. 2,06
Duration of Single Impulse, s….. 0,050.. .3000
Nozzle Expansion Ratio….. 150
Maximum Thruster Length, mm (in) ….. 600
Maximum Nozzle Diameter, mm (in) ….. O226
Maximum Mass, kg (Ibm) …..3,5
Cycle Life, Number of starts-up …..150000
Nominal Voltage, VDC….. 27
Voltage Range, VDC …..20…34