Products
R&D
- Integrated Fuel-Air HX for Turbine Engines
- Cryo HX w/Anisotropic Conductance
- Advanced Turbine Blade Cooling
- Small Rocket Motors
Services
Microchannel-Cooled Rocket Components
Ni rocket motors, before and after machining |
In earlier work, Micro Cooling Concepts' employees developed a microchannel-cooled rocket combustor using LOX as the coolant. The combustor, shown below, had a 7.5"-tall chamber with a 2.5" inner ID. 62.5 micron microchannels lined the entire inner surface.
Similar approaches can be used for throats and nozzles.