MR-106L 22N

MR-106L 22N image

Overview

MR-106L 22N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.59 kg, with a specific impulse of 228 to 235 sec and a thrust of 10 to 34 N (steady state).

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Overview

Name
MR-106L 22N
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
Aerojet Rocketdyne
Founded
1942

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Specifications

Form Factor
SmallSat
Dry Mass
0.59 kg
Average Power
36.16 W
Heritage
Yes
Status
In Production
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