jmshiloh
Mechanical
- Jan 14, 2003
- 1
I'm part of a group of hobbiests who make ther own model rocket engines. We have been using graphite for nozzles. It is quite expensive and needs to be machined.
I found a material from Contronics in NJ called Rescor 770. It is a 2 part (powder and activator/resin) castable silicon carbide ceramic. It is lower in cost than graphite and moldable at room temperature as well. However, it is still too expensive at about $10 per pound.
Does anyone have a recommendation for a suitable castable ceramic of either tungston or silicone carbide. The material will have to be castable at room temperature, However, post curing at elevated temperatures is OK (hopefully not at kiln levels).
We have tried pourstone concrete anchoring material and it works fairly well. However, it erodes and degrades motor performance. The actual working pressure in an engine can exceed 1000-2000psi.
Tha actual nozzle is 2" in diamter X 2" long and is held in the motor casing by a snap ring around the front face of the nozzle. Combustion gas temeratures can exceed 3500C for periods of 10 seconds or less.
I found a material from Contronics in NJ called Rescor 770. It is a 2 part (powder and activator/resin) castable silicon carbide ceramic. It is lower in cost than graphite and moldable at room temperature as well. However, it is still too expensive at about $10 per pound.
Does anyone have a recommendation for a suitable castable ceramic of either tungston or silicone carbide. The material will have to be castable at room temperature, However, post curing at elevated temperatures is OK (hopefully not at kiln levels).
We have tried pourstone concrete anchoring material and it works fairly well. However, it erodes and degrades motor performance. The actual working pressure in an engine can exceed 1000-2000psi.
Tha actual nozzle is 2" in diamter X 2" long and is held in the motor casing by a snap ring around the front face of the nozzle. Combustion gas temeratures can exceed 3500C for periods of 10 seconds or less.