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John R Weiss wrote:
"John S. Shinal" wrote... Cyclic ops - CTOL has long operated with tightly timed launches and deployments - do you launch and recover CTOL a/c together and STOVL together, but never mix types ? For timing purposes, it shouldn't be much different than a mixed A-6 / F-4 or F-14 / F-18A/B flight deck -- the cycle time is controlled by the shortest endurance. In the case of the former, there was enough organic tanker support to keep the F-4s alive for a 1+45 cycle. In the latter case, the F-18s dominate, and normal cycle times are reduced to 1+30 or less. When you come to a F-18 / F-35 STOVL loadout, there could be a LOT of F-18 tankers supporting 1+30 cycles for the F-35, or the cycle times will be reduced to 1+15 or less. snip Don't see why. The F-35B will have considerably more internal fuel than an F-18A-D with similar weight, a single engine and no need for 3-5,000 lb. of recovery fuel reserve. Marine profile mission radius (KPP) is 450nm from a 550' STO (590nm for the USAF F-35A mission profile; 600nm for the USN F-35C mission profile), with a VL bringback of .2 x 1k JDAMs and a pair of AIM-120s, plus reserve fuel. Guy |
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Thread | Thread Starter | Forum | Replies | Last Post |
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