Review Article

Development of Electric and Chemical Microthrusters

Table 2

Summary of micropropulsion key performance parameters.

Electric micropropulsionChemical micropropulsion
Single FEEPmN-FEEPμPPTBipropellant Monopropellant

Size (cm) ~5 cm ~10 cm~  mm ~3 cm ~2.5 cm
~10 cm ~10 cm ~7 cm ~5 cm
Mass (kg)80 g thrusters + 700 g PCU300g thruster + 1 kg PCU<0.2 (4 units incl. PCU)<0.1<0.06 g
Power (W)0.5 (heater)7 (heater)1-2<3 (valves)<1.5
(s)>5,000>4,000>500290–330153
Total impulse (Ns)>30 >600 50–500>5000>2000
MIB (μNs)<5 × 10−3<5 × 10−310–30
Thrust0.1–15 μN0.1–300 μN~10 μN1–3 N150–900 mN
PropellantIndiumIndium or GalliumTeflonEthanol, RP-1;
H2O2 (87.5%)
H2O2 (87.5%)
Feed/operating Pressure (bar)Self-feedingSelf-feedingN/A6–12 bar3–6 bar
Flow/consumption Rate (g/s)(depends on thrust)(depends on thrust)N/A0.2–1 g/s0.1–0.4 g/s
Pulse rate (Hz)>50 Hz >50 Hz 0.5–3TBDTBD
Pulse duration (s) ~10 μsTBDTBD
Exit diameter4–8 mm4–8 mm~  mm15 mm5 mm
Beam power-to-thrust ratio (W/mN) 50 80 N/AN/AN/A
Thrust efficiency>50%>50%
Technology readiness level (TRL)63333

Depends on reservoir size and number of LMISs in cluster.
Depends on power supply.
Excluding PCU losses and heater.