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On Wed, 08 Oct 2003 19:46:27 GMT, Guy Alcala
wrote: On that note, anyone got any idea of how much did the A7s long long legs reduce by when fitted with the bigger blower ? The A-7F, Corasair III, Strikefighter, etc. all included an airframe stretch and extra fuel in addition to an F100 or F110. Interesting, I didnt know about the F110 being considered for it. The airframe stretch was to allow the a/c to be supersonic (Mach 1.4 level IIRR), and the extra fuel was to keep the range/endurance in the same ballpark. Any idea of the peformance improvement on the 'lo' part of an attack mission with the F110/F100 ? For instance, here's the proposed Corsair III changes, which was designed to use rebuilt A-7A/A-7B airframes from the Boneyard, although A-7D/Es would be easier to convert: An F110-GE-100, 16,700 lb. mil and 27,600 lb. A/B; A constant-section plug of 29.5" to extend the fuselage around the wing root area; another plug of 7.5" to the aft fuselage to tailor the airframe to the F110 and its remote accessory gearbox. Rear fuselage canted upwards 5 degrees to provide ground clearance for the longer tailpipe. A more sharply-pointed nose cone (see F-8); the original was made blunter to reduce length on carriers. Internal configuration changed to increase fuel capacity. Did the USN have any interest in looking at a turbocharged E model ? greg -- $ReplyAddress =~ s#\@.*$##; # Delete everything after the '@' The Following is a true story..... Only the names have been changed to protect the guilty. |
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