MR-104H 510N

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Overview

MR-104H 510N is a flight proven hydrazine monopropellant thruster. The thruster has a total mass of 2.40 kg (includes engine and valves), with a specific impulse of 223 to 237 sec and a thrust of 201.0 to 554.2 N (steady state).

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Overview

Name
MR-104H 510N
Form Factor
SmallSat
Heritage
Yes

Vendor Details

Name
Aerojet Rocketdyne
Founded
1942

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Specifications

Form Factor
SmallSat
Dry Mass
2.4 kg
Average Power
60.1 W
Heritage
Yes
Status
In Production
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