Propellants, Fuel/Oxidizer…..UDMH/NTO
Mixture Ratio …..1.85+0.05
Average Nominal Thrust, N (Ibf) ….. 196 (44.06)
Average Specific Impulse, Steady State, sec….. 307
Nominal Inlet Pressure, MPa (psi) ….. 2.06 (298.78)
Duration of Single Impulse, s …..0.037... 2,000
Nozzle Expansion Ratio….. 100
Maximum Thruster Length, mm (in) ….. 376 (14.80)
Maximum Nozzle Diameter, mm (in) ….. O 126 (4.96)
Maximum Mass, kg (Ibm) …..2.0(4.41)
Cycle Life, Number of starts-up….. 250 000
Nominal Voltage, VDC….. 27
Voltage Range, VDC….. 20...34