mixdenny
Cast Iron
- Joined
- Feb 5, 2005
- Location
- North Olmsted, Ohio
These pictures are from 1951 and 1953.
This last picture is one I am quite familiar with. He is working on an inner liner for a small rocket nozzle, I would guess about 2,000-5,000 lbs thrust. The nozzle is built of a copper alloy called NASA-Z. You can see the many cooling passages that the liquid hydrogen flows through. This keeps the nozzle from burning up and pre-heats the fuel. Each passage is a constant cross-sectional area, so as the diameter of the nozzle gets smaller, each passage goes from a wide, shallow groove to a narrow, deep groove in a continuous smooth transition. After the grooves are machined, they are filled with wax, then the entire nozzle goes in a nickel plating tank and is completely sealed with an outer layer of nickel that ends up about 1/2" thick, it takes weeks to plate it that much.
At the throat, the grooves are very deep and the remaining copper wall is only 0.010" thick to get good heat transfer to the fuel. The fuel is pressurized to the same pressure as the combustion chamber is running, usually 1000 to 2000 psi, so there is no pressure differential across the walls. We developed the high pressure Lox-hydrogen motor at Lewis. I worked with the engineer who held the patents for developing the solid-electroplated nozzles. Before that each engine was built up of hundreds of formed nickle tubes all wrapped with steel wire and the whole thing furnace brazed together. The Space Shuttle main engines are all electroplated to solid using our technique. In order to achive the maximum heat transfer at their throat, the inner surface is gold plated. Dennis
This last picture is one I am quite familiar with. He is working on an inner liner for a small rocket nozzle, I would guess about 2,000-5,000 lbs thrust. The nozzle is built of a copper alloy called NASA-Z. You can see the many cooling passages that the liquid hydrogen flows through. This keeps the nozzle from burning up and pre-heats the fuel. Each passage is a constant cross-sectional area, so as the diameter of the nozzle gets smaller, each passage goes from a wide, shallow groove to a narrow, deep groove in a continuous smooth transition. After the grooves are machined, they are filled with wax, then the entire nozzle goes in a nickel plating tank and is completely sealed with an outer layer of nickel that ends up about 1/2" thick, it takes weeks to plate it that much.
At the throat, the grooves are very deep and the remaining copper wall is only 0.010" thick to get good heat transfer to the fuel. The fuel is pressurized to the same pressure as the combustion chamber is running, usually 1000 to 2000 psi, so there is no pressure differential across the walls. We developed the high pressure Lox-hydrogen motor at Lewis. I worked with the engineer who held the patents for developing the solid-electroplated nozzles. Before that each engine was built up of hundreds of formed nickle tubes all wrapped with steel wire and the whole thing furnace brazed together. The Space Shuttle main engines are all electroplated to solid using our technique. In order to achive the maximum heat transfer at their throat, the inner surface is gold plated. Dennis