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in service until 1988...debut in 1960
Well, Waynos, 28 years in service sounds good to me. What is sad is that there was not a follow up aircraft to the Lightning since the company seemed to be solving problems in rather unique ways. The upper engine was behind the lower one which meant a lower cross section because the inlet diameter is less than the overall diameter. Apparently it could go supersonic without reheat which was kind of rare back then. It looks like an exceptionally good aircraft to me.
Even worse than the Starfighter!? Crikey!Why was that then, was it because it lacked flaps and most accidents happened at landing?
Hard to say - I know Denmark operated them and also lost many. I think it might of been training and the mission.
Ground effects. The F-100 was aerodynamically prone to it. If the nose was rotated slightly above "textbook" take-off restrictions it would float on a cushion of air it compressed between itself and the ground. Once there it was like rolling on a balloon and ultimately falling off. At that angle of attack the wing was not generating adequate lift nor was there enough power to horse it into flight.
View: https://www.youtube.com/watch?v=iOamnWpLtO8
Interesting info, never heard that but I wouldn't immediately dismiss it, I'll ask some old timers I know. I'll be in Ca next week by EDW.Sweb, I can't vouch for the authenticity of my statement, but it was told to me by a Nam vet who was a C130 driver. He claimed that video was from a maintenance SNAFU from improperly rigged ailerons. As the story went, he said the Huns original aileron rigging were equal length and they were cross-rigged. Post accident findings resulted in design guideline "best practices" to make all opposing flight control rigging of unequal length to prevent such Class A's from occuring in the future. If anyone has any info on the validity of this story, I would love to hear it. [FBJ?]
Ground effects. The F-100 was aerodynamically prone to it. If the nose was rotated slightly above "textbook" take-off restrictions it would float on a cushion of air it compressed between itself and the ground. Once there it was like rolling on a balloon and ultimately falling off. At that angle of attack the wing was not generating adequate lift nor was there enough power to horse it into flight.
View: https://www.youtube.com/watch?v=iOamnWpLtO8
It was a treat to watch the F-106s take off at dawn or dusk. The afterburner was something.
Back at Griffiss AFB I built a 1/72 scale F-106 in 49th Markings. I have the kit and decals to do a 1/48th one. I love that plane! The only thing is I want to do the tail number for the one at the Air Force Museum. That is the one that the pilot ejected from in Montana. And the pilotless plane recovered from the flat spin and landed with little damage in the snow!
Bill G.
I think you meant J-58'sThe F-22's engines generate more than 35K lbs thrust each in AB. That's more than the static thrust of the SR-71's J-85's.
It did IMO.I've read that the ramjet-bypass system of the SR-71 generated more thrust than the J-58s themselves at high speed. Does this mean that the Blackbird had more than 64,000 lbs thrust on tap at M.3+?
I can't seem to find anything specific in regards to this.
JL
How did the Delta Dart and Delta Dagger stand in comparison back in the day?
nope exactly the same mission Bear hunting over the pond.Different mission.