Propellants, Fuel/Oxidizer….. O2(gas)/kerosene
Average Nominal Thrust, N (Ibf) …..186.40 (40.85)
Average Specific Impulse, Steady State, sec …..257
Nominal Inlet Pressure, MPa (psi) ….. 3.43/1.62 (497.47/)
Maximum Inlet Pressure, MPa (psi) ….. 5.89/1.96 (852.81/284.27)
Minimum Inlet Pressure, MPa (psi) …..2.45/1.37 (355.34/199.00)
Minimum Impulse Bit, N-s (Ib-s) …..  11.2 (2.52)
Duration of Single Impulse, s….. 0.06-100
Nozzle Expansion Ratio …..52.9
Maximum Thruster Length, mm (in) ….. 360 (14.17)
Maximum Nozzle Diameter, mm (in) ….. 094 (3.70)
Maximum Mass, kg (Ibn,) …..6.3(13.9)
Total Impulse, kN-s (kib-s) 857.4….. (193.02)
Cycle Life, Number of starts-up….. 40,000
Nominal Voltage, VDC …..27
Voltage Range, VDC….. 23...34
Pull-in Current, A….. 0.05/0.2...0.3
Holding Current, A….. 0.02/0.1