I am researching early U-2 versions, and I bumped into something strange. All my sources (Aerograph, In Action, Blackbirds, various websites) report that:
- the U-2A had the J57-P31A engine
- the U-2B had the J75-P13 engine using the same inlets as the U-2A
- the U-2C had the J75-P13B engine and much inlarged inlets
I always found the combination of J75 and small inlets strange, I wouldn't expect that the mass flow would match. But each and every source says the B had the J75. That is, until I found a document on the CIA website called "The CIA and the U-2 program, 1954 - 1974", dated 1998:
Who is right here?? The CIA version makes more sense to me, but it stands alone. Are my other sources possibly outdated (they are all some 15 years old) ?
Rob de Bie
PS: The document contains numerous other juicy bits, like maps of Russian and Cuban overflights (p107, p202), the steadily decaying number of Agency U-2's (p251 reports 6 left in 1966, of the 20), the blue-black color (p149), etc. Recommended!
My models: