MR-401 0.09N

MR-401 0.09N image

Overview

MR-501 0.09N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 0.60 kg, with a specific impulse of 180 to 184 sec (steady state) and a thrust of 0.07 to 0.09 N (steady state).

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Overview

Name
MR-401 0.09N
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
Aerojet Rocketdyne
Founded
1942

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Specifications

Form Factor
SmallSat
Dry Mass
0.6 kg
Average Power
11.95 W
Heritage
Yes
Status
In Production
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