NANO - ENPULSION - SmallSat Catalog - Orbital Transports
Additional Information
Type:
Electric Propulsion
Nominal Thrust:
330 µN
Specific Impulse:
2,000 to 6,000 s
Dynamic Thrust Range:
10 to 350 µN
Total Impulse:
>5,000 Ns
Maximum Power Consumption:
40 W
Dimensions:
100 x 100 x 82.5 mm
Dry Mass:
680 g
Wet Mass:
900 g
Propellant mass:
220 g
Interface:
RS422
Interface:
RS485
Supply Voltage:
12 V
Supply Voltage:
28 V
Operating Temperature:
-20C to 40C
Survival Temperature:
-40C to 105C
Documentation

Electric propulsion thruster for nano- and micro-satellites based on the mature and proven FEEP technology. The ENPULSION NANO can also be clustered in different configurations. More than 60 ENPULSION NANO thrusters have been deployed in space as of April 2021.

ENPULSION NANO

ENPULSION
Description

Electric propulsion thruster for nano- and micro-satellites based on the mature and proven FEEP technology. The ENPULSION NANO can also be clustered in different configurations. More than 60 ENPULSION NANO thrusters have been deployed in space as of April 2021.

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Additional Information
Type:
Electric Propulsion
Nominal Thrust:
330 µN
Specific Impulse:
2,000 to 6,000 s
Dynamic Thrust Range:
10 to 350 µN
Total Impulse:
>5,000 Ns
Maximum Power Consumption:
40 W
Dimensions:
100 x 100 x 82.5 mm
Dry Mass:
680 g
Wet Mass:
900 g
Propellant mass:
220 g
Interface:
RS422
Interface:
RS485
Supply Voltage:
12 V
Supply Voltage:
28 V
Operating Temperature:
-20C to 40C
Survival Temperature:
-40C to 105C
Documentation

Electric propulsion thruster for nano- and micro-satellites based on the mature and proven FEEP technology. The ENPULSION NANO can also be clustered in different configurations. More than 60 ENPULSION NANO thrusters have been deployed in space as of April 2021.