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I have to say that Koopernic's post #79 of this blog is the first detailed description of a German AA artillery VT fuze I have read in the literature or in the net. Until now most of the sources I have seen just rely on a vanished (?) CIOS report mentioning Kuhglöckchen as electrostatic influence fuze without technical details. Even Fritz Trenkle does not tell anything about it in his books.
Unfortunately Koopernic does not seem to be active in this forum anymore. Does anybody know more about the original source of his description?
When you say "orienting the parts structurally" you mean putting the strongest parts in the places where the most strength is required?I was curious about the tube technology used in VT fuses. Apparently they did various ruses in design by orienting the parts structurally and filling the tubes with wax!
loads from the not inconsiderable rotational forces generated.
The question I have is: If we had proximity fuses that could take such enormous g-loads, and some were fitted to rockets -- why did we have so many guidance system failures during Vietnam?
Most were caused by the following
I'm curious how these conditions would compare to conditions in territory that was controlled by the United States itself. I assume our test-facilities were on the base themselves, with air-temperature and humidity varying with location. I'm not sure how TAC & SAC varied in terms of maintenance -- SAC generally was more anal about things being done exactly right, but I'm curious if mistakes were made.
- Dropping: Sometimes, when the missiles were put on the wings, or fuselage of the aircraft, they'd drop off and hit the ground. In cases where the missile didn't have any denting or damage to fins or shape, they would often just send the plane on it's way. I'm not sure what g-load a missile hitting the ground after dropping a few feet off an aircraft's wing or fuselage would be, but it seems quite a lot less than 5,000-8,500g on the low end to up to 20,000g on the upper end of things. I've fallen about 10-20 feet, and I figure if I had been subjected to these g-loads, I'd be mist.
- Jarring: Basically, the missiles were often carried on trucks that lacked shock-absorbers. The fact that the testing facilities were not on the base, and sometimes located at separate facilities, where they would have to travel across bumpy roads, and things of that sort. To make it worse, air-bases often had these washboard structures meant to shake off FOD.
- Temperature: The missiles at sea-level were in warm/hot weather, and temperatures that were -20F to -70F at around 15000 to 40000 feet where you'd typically see fighter planes operating within. The result of temperature is contraction and expansion, and different components expand/contract at different rates. As a result, sometimes missiles would pass electronic inspection, then fail spectacularly in the air.
- Corrosion: The air in Vietnam was hot and moist, which can accelerate corrosion on aircraft operating with the USAF and USMC; the USN operated off carriers in the salty-air at sea. I'm not sure what the protocols for missile assembly were, but I'm curious if the missiles in either case were left partly assembled in the open.
From memory, I can look up a passage in the book if you like, the earlier for example 45 fuzes used a perspex/plexiglass body (insulator), a tung bean oil "potting" and a can, an actual cylinder of tin, in side which the tubes were located.I was curious about the tube technology used in VT fuses. Apparently they did various ruses in design by orienting the parts structurally and filling the tubes with wax! A lot of genius in design, persistence and technical capability expended here! It was done by never say impossible types!