250N Monopropellant Thruster

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Description

A 225 N monopropellant engine developed by Space Solutions. The thruster the propellant H2O2, has a mass of 0.85 kg, and a specific impulse of 170 seconds.

 

Datasheet

Space Solutions – 250N Monopropellant Thruster

Overview
Name250N Monopropellant Thruster
ManufacturerSpace Solutions
SubsystemPropulsion
ClassificationMonoprop Thruster
Form FactorSmallSat
Vendor Overview
Vendor NameSpace Solutions
Vendor Websitehttp://www.spacesolutions.co.kr/
Vendor LocationKorea
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    SPECIFICATIONS
    SubsystemPropulsion
    ClassificationMonoprop Thruster
    Form FactorSmallSat
    VendorSpace Solutions
    HeritageN/A
    Mass0.85 kg

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