Propellants, Fuel/Oxidizer….. UDMH/NTO
Mixture Ratio …..1.85±0.15
Average Nominal Thrust, N (lbf) ….. 130.5 (29.34)
Average Specific Impulse, Steady State, sec….. 306
Nominal Inlet Pressure, MPa (psi) ….. 2.06 (298.78)
Duration of Single Impulse, s….. 0.030...2,000
Nozzle Expansion Ratio….. 100
Maximum Thruster Length, mm (in) …..376 (14.80)
Maximum Nozzle Diameter, mm (in) ….. O126 (4.96)
Maximum Mass, kg (Ibm) ….. 1.8(3.97)
Cycle Life, Number of starts-up….. 500,000
Nominal Voltage, VDC …..27
Voltage Range, VDC….. 21.. .34