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#101
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On Wed, 02 Jun 2004 08:03:20 -0500, Pat Flannery
wrote: I want to know what the "cheek bulges" on the side of the forward fuselage are all about. ....Mumps. OM -- "No ******* ever won a war by dying for | http://www.io.com/~o_m his country. He won it by making the other | Sergeant-At-Arms poor dumb ******* die for his country." | Human O-Ring Society - General George S. Patton, Jr |
#102
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In article ,
Pat Flannery wrote: I want to know what the "cheek bulges" on the side of the forward fuselage are all about. If memory serves, the Crusader had a single bulge -- one side only -- because its otherwise quite skillful designers had somehow neglected to provide space for a retractable flight-refueling probe, and somewhere between the design freeze and the production order, the USN decided to insist on having one. -- "Think outside the box -- the box isn't our friend." | Henry Spencer -- George Herbert | |
#103
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On Wed, 2 Jun 2004 22:41:11 +0800, "Neil Gerace"
wrote: "OM" om@our_blessed_lady_mary_of_the_holy_NASA_researc h_facility.org wrote in message ... ...For some reason when I look at that damn thing, the word "seagull" pops into my mind, and I suddenly have an urge to throw a few dozen Alka-Seltzers in the intakes :-P Do Alka-Seltzers cause seagulls to explode? Must give that a go next time I'm at the cricket. ....That's the myth. The truth is that it inflates their stomach to the point that the pain prevents them from flying, and they auger fatally into the drink. OM -- "No ******* ever won a war by dying for | http://www.io.com/~o_m his country. He won it by making the other | Sergeant-At-Arms poor dumb ******* die for his country." | Human O-Ring Society - General George S. Patton, Jr |
#104
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![]() "OM" om@our_blessed_lady_mary_of_the_holy_NASA_researc h_facility.org wrote in message ... On Wed, 2 Jun 2004 22:41:11 +0800, "Neil Gerace" wrote: Do Alka-Seltzers cause seagulls to explode? Must give that a go next time I'm at the cricket. ...That's the myth. The truth is that it inflates their stomach to the point that the pain prevents them from flying, and they auger fatally into the drink. That doesn't sound like a nice way to die ![]() those flying water rats. |
#105
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#106
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#107
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On Tue, 01 Jun 2004 01:37:57 -0500, Pat Flannery
wrote: Mary Shafer wrote: Someone asked about a refueling receptacle back by the tail on the F-8. First, receptacles are on the forebody, not at the back end. Secondly, the F-8, being a Navy airplane, has a probe, not a receptacle. It's on the left side, just below the cockpit, I think. I think it was a reference to a ground refueling point; but it clearly is hydraulically related given the writing on the data placard. It wouldn't be on the top, up at the back. The Crusader is a Navy airplane, operated off carriers. The Navy doesn't make the mechanics climb up and stand on the airplane to refuel it, because even super carriers develop quite a lot of deck motion in high sea states. We put a flight control computer in that space, after removing the probe, on our F-8, so I'm going by memory of the dummy probe we strapped onto the airplane for my PIO suppression filter testing. Ever see the cool looking supercritical wing test F8? Or is this the one you are referring to? Naturally. It's parked on a concrete pad right beside my F-8, which was the Digital Fly-By-Wire. They're both F-8Cs that we got from the Navy. In fact, we asked for an F-8 for the supercritical wing. We also had some plans to put a skew wing on the F-8 DFBW, jointly with the Navy. Because all you have to do is disengage the jack screw at the front of the wing and remove the pin from the hinge at the back to lift the entire wing structure right off, the F-8 is a natural for putting new wings onto. Using the DFBW would have let us use a flight control system that greatly reduced the cross-axis effects (pitch maneuvers causing roll and yaw movements and vice versa). This would have been a transonic airplane and the major advantage of the skew wing would have been the reduction in spotting factor. The skew wing spotting factor would have been 0.7, while a regular F-8 had a spotting factor of 1.3 (I think the A-4 was still the standard, although it may have been the A-7). That's a substantial reduction, one that the Navy would really like to see. But Dryden and the piece of the Navy advocating this couldn't get approval at the higher levels of our respective agencies, so we never did it. Mary -- Mary Shafer Retired aerospace research engineer |
#108
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On Tue, 01 Jun 2004 21:18:49 GMT, Doug...
wrote: Also, recall that several different types of planes have been used as unmanned drones in target practice over the Southern California desert. Not only do you need to test new weapons, to make sure they'll work properly, you also need to train crews on the actual use of these weapons. Which means you occasionally need to be able to shoot down real jets. This isn't done just anywhere, though. You have to have a range that you can drop big chunks of airplane on without smashing houses, cars, livestock, and people. The Navy does it at China Lake, as part of their missile testing. They're using QF-4s right now. If the USAF uses drones, it's probably only at Eglin. Does anyone know if the Crusader was ever used regularly in drone service? I don't think so, because we sold them to the Philippines. They even took the F-8B, which was at Dryden. It was a two-seat airplane but its biggest distinction was that it was the last US fighter with a pushrod and cable flight control system. Mary -- Mary Shafer Retired aerospace research engineer |
#109
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On Wed, 02 Jun 2004 00:30:04 -0500, Pat Flannery
wrote: Some F8A's were converted as drone control aircraft as DF8L's, but I haven't found any info on ones that were converted to target drones as such. I think you mean QF-8L. The designator for drones is Q and the hyphen is part of the reformed designations system, which was put in place just before the F-8 came online. Mary -- Mary Shafer Retired aerospace research engineer |
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