Search results

I'm assuming you mean GE's F110 Engines fitted to later blocks of F-15E's, F-16's and F-14B/D's, then taking it as a starting point, and if you are developing a new core and fan section as well the dry thrust target should be around 230000-25000lbf or 102kN to 111kN with the current available...

Not exactly, one can always scale or use an existing core to develop an engine for a different role, one example is GE's F101 Engine. Designed solely for the B-1 Lancer, the company later used the core of the engine for their later joint venture engine with SNECMA (now SAFRAN Aircraft Engines)...

Nope, RR is very active on the commercial side as well, and they are already testing Ultrafan. While there maybe a difference between a civilian high bypass turbofan and a military oriented low bypass turbofan, I'm sure RR can always adapt the core architechture of a civilian engine and make a...