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.
Engine info.
Thrust: 3,8 ton
Fuel: Ethanol - Hydrogen peroxide H2O2 (85-90%)
Fuel consumption: 4,15 kg/s
Oxidant consumption: 8,55 kg/s
Isp: 220
Isp: 220
Pressure in COP: 5,4 MPa
Engine plate thickness: 3 mm
Engine length: 834 mm
Materials: Stainless steel
In any static ground testing and also in the flight, we collect data from various points on the engine. Here are some of them.
- Thrust (lb)
- Thrust (lb)
- Chamber pressure (psi)
- Igniter temperature
- Jet vanes temperature
- Jet vanes downward force
- Jet vanes downward force
- Fuel consumption (LOX and Ethanol)
- Alcohol fuel temperature
- Alcohol fuel level in cooling passage (Prime)
- Ambient temperature