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HTP3Z-1X bi-Liquid fuelled regenerative cooled
HTP3Z-1X bi-Liquid fuelled regenerative cooled. The HTP3Z-1X bi-liquid rocket engine is the latest in engines at Sweden Rocket Research Group. HTP3Z-1X runs on a fuel mix of ethanol - Hydrogen peroxide and it has a thrust of 3,8 ton. The first generation of the HTP3Z-1X engine is primarily a test article. Thrust 3,8 ton. Fuel Ethanol - Hydrogen peroxide H2O2 85-90. Fuel consumption 4,15 kgs. Oxidant consumption 8,55 kgs. Pressure in COP 5,4 MPa. Engine plate thickness 3 mm.
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HTP3Z-1X bi-Liquid fuelled regenerative cooledDESCRIPTION
HTP3Z-1X bi-Liquid fuelled regenerative cooled. The HTP3Z-1X bi-liquid rocket engine is the latest in engines at Sweden Rocket Research Group. HTP3Z-1X runs on a fuel mix of ethanol - Hydrogen peroxide and it has a thrust of 3,8 ton. The first generation of the HTP3Z-1X engine is primarily a test article. Thrust 3,8 ton. Fuel Ethanol - Hydrogen peroxide H2O2 85-90. Fuel consumption 4,15 kgs. Oxidant consumption 8,55 kgs. Pressure in COP 5,4 MPa. Engine plate thickness 3 mm.CONTENT
This web page rd1xengine.blogspot.com states the following, "The HTP3Z-1X bi-liquid rocket engine is the latest in engines at Sweden Rocket Research Group." We saw that the webpage said " HTP3Z-1X runs on a fuel mix of ethanol - Hydrogen peroxide and it has a thrust of 3,8 ton." It also said " The first generation of the HTP3Z-1X engine is primarily a test article. Fuel Ethanol - Hydrogen peroxide H2O2 85-90. Fuel consumption 4,15 kgs. Oxidant consumption 8,55 kgs. Pressure in COP 5,4 MPa. Engine plate thickness 3 mm."SEEK SIMILAR DOMAINS
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