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There was also the U.K. based Nimbus 4 in Spain.
The ASW20CL on 11th January 1987 was an overspeed accident. It did not break up, control was lost and it hit the ground at very high speed. I should have thought there was a case for an optional tail chute on machines such as the big Nimbus and perhaps the Duo Discus, it was fitted to the Janus and the Nimbus 2. The ASW17 was available with a belly chute. W.J. (Bill) Dean (U.K.). Remove "ic" to reply. "Andreas Maurer" wrote in message ... On 28 Mar 2004 22:53:07 GMT, John Galloway wrote: Through the contributions to the avoiding VNE thread runs the theme of the difficulty of avoiding overspeeding and/or overstressing some modern designs in accidental spin recovery. This is made more difficult than in older composite gliders because they had a little more drag and a little more (fortuitous) margin in the g limits. Is it not blindingly obvious that there is a need for an emergency drag device that does not reduce the G limits of gliders? Clearly if we all handled the recovery from inadvertent spins etc perfectly all would be well but equally clearly that does not always happen and it is a shame to lose pilots in this situation. Well, I have to admit that as fine as your solution sounds - it will only be the cure for an extremely small part of all glider accidents. How big is the fraction of overspeed/overG accidents after a spin recovery that went wrong? 0.1 percent? 0.2 percent? Certainly not higher - the only inflight breakups in such a situation I ever heard of were the ASW-22 prototype (1981), the eta and the US Nimbus, the first two being test flights of prototypes. In the 22 case it was clear that the airframe would break up before the flight because it was not designed for the load factors that were created by extreme asymmetrical water ballast load. Bert Willing also exceeded the design limits of a 26 meter glider, but his glider survived the incident without damage. Investing a very small part of the costs for such a device in, say, three spin-training flights per year, is probably going to make things a lot safer. I think the money is far better invested in a rescue system, be it NOAH, bee it Soteira (which I prefer), or be it a BRS. A rescue system will be able to safe the pilot in a lot more cases than a strong airbrake. Bye Andreas |
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