2500N Bipropellant Engine

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Description

Space Solution’s 2500 N bipropellant thruster has a specific impulse of 293 seconds with a chamber pressure of 20 bar. The thruster is designed to use H2O2 90% wt / kerosene.

 

Datasheet

Space Solutions – 2500N Bipropellant Engine

Overview
Name2500N Bipropellant Engine
ManufacturerSpace Solutions
SubsystemPropulsion
ClassificationBiprop Thruster
Form FactorSmallSat
Vendor Overview
Vendor NameSpace Solutions
Vendor Websitehttp://www.spacesolutions.co.kr/
Vendor LocationKorea
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    SPECIFICATIONS
    SubsystemPropulsion
    ClassificationBiprop Thruster
    Form FactorSmallSat
    VendorSpace Solutions
    HeritageN/A

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