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The General Electric AC110-2 Nuclear Turbojet was selected by Convair in 1956 to power their Models 23A and 23B nuclear seaplane bombers / mine layers. Layout of the AC110-2 is very similar to the GE XMA-1A, with a single reactor for each pair of turbojets (one pair in the 23A, two pairs in the 23B).
My questions are:
• Does anybody have some documentation on the GE AC110-2 (reactor MW, engine thrust, etc.)?
• Is this engine design before or after the GE XNJ140E?
Don't worry about the NSA -- you can probably speak freely.
My questions are:
• Does anybody have some documentation on the GE AC110-2 (reactor MW, engine thrust, etc.)?
• Is this engine design before or after the GE XNJ140E?
Don't worry about the NSA -- you can probably speak freely.