could be...the MATS page suggests all initial terms were met. but it doesn't go into much detail on each individually.
oh, here's another (3rd & 4th paragraphs): http://www.anft.net/f-14/f14-h...
"With its 65,000 lbs of thrust, the F101DFE engines produced enough power to give the F-14 a thrust to weight ratio of almost one to one. That means, the F-14B prototypes were able to accelerate in the vertical, something the F-14A was unable of. But the Navy - not the pilots - decided against the F-14B and the test program was terminated in September 1981.
A few years later, in July 1984, Grumman was ordered to take the F-14B prototype out of storage again and install a pair of General Electric F110-GE-400 engines..."
same source again though, so my diversity is low. so far that's the most comprehensive f14 page i've found, but i can't say with any authority how accurate it is.
been chatting about it allot on Falcon BMS forums lately. you know the f14 seems like it might have had the worlds first microprocessor as well: http://www.firstmicroprocessor...