- Reaction score
- 0
- Points
- 160
benny88 said:Has this been decided? I understand the desire for an internal gun, but I was under the impression that the more robust landing gear, tail hook, and folding wings were advantageous for how we operate our fighter fleet, and I believe there's an advantage in range as well, based on both more fuel and larger wing area.
Not entirely sure that I understand your question, so if my answer is inaccurate please let me know.
The F-35A variant is the one being pursued by the Government at this time. The plane will come armed with a GAU-12 Equalizer 25 mm cannon and has planned add ons which include the addition of a drag chute which will be situated at the rear of the aircraft between the tail fins as well as a refuelling probe at the nose of the aircraft similar to that being placed on the B/C variants.
According to data released regarding performance standards, the A model has the same wing area (42.7m square) as that of the B which is less than that of the C model (62.1m square). The A model has a greater internal fuel capacity (8,390kg vs. the 6,030kg of the B model) and as a result it also has both a greater range (2,220km vs. 1,670km) and a greater combat radius based on internal fuel (1,090km vs. 833km) respectively.
Neither variant (A/B) has the size/range/combat radius of the C version which is being designed specifically for US carrier operations. As well, the notion that folding wings are advantageous for how we operate our fighter fleet isn't really a consideration given that we do not perform carrier based operations where wing folding is necessary to ensure maximum space utilisation in a finite area.
Hope that helps...??