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|    Message 185,493 of 187,313    |
|    Jim Wilkins to All    |
|    Re: Boeing Space Ships. The name goes on    |
|    03 Jul 24 08:31:40    |
      XPost: or.politics, alt.politics.trump, alt.fan.rush-limbaugh       XPost: alt.astronomy, rec.aviation.military       From: muratlanne@gmail.com              "R Kym Horsell" wrote in message       news:v62l3f$1r7h$4@nnrp.usenet.blueworldhosting.com...              According to the contract they had to test them in a certain way the       company officials considered a big old waste of time and money.       If a fauly was detected the whole test rig was SUPPOSED to be shut down       and colled off, then re-started and the controller had to the get up       to speed then pass the test. The company method was to just keep going       until the controller passed the tests and ignore any failures along the way.              ------------------------------              I was in the industrial testing business for a while. "Test until pass"       wasn't an uncommon practice, there's enough random variation in repeated       test results to somewhat justify it, and the fail limit may be arbitrarily       overcautious. It may have been set by Marketing to look good on a spec       sheet, and you won't go to jail for setting it too high but you might for       setting it too low. When weight doesn't matter much the safety factor is       typically at least 3 to 5, while in aviation it may be 1.5. For the steel       chain I just bought it's either 3 or 4 depending on grade, I don't know why       the difference. Chain rated to hold 6600 Lbs in use is tested during       production at 13,200 and expected to break at 26,400.              In one case I found a timing bug in the test station's computer microcode       that caused occasional failures which didn't repeat when the part was       retested, so passing it through a second time was the procedure. The test       was the problem, not the component. My reward was being assigned to a new       product's development team. Unfortunately such small highly specialized       companies go broke or at least lay off the engineering staff when capital       investment in new equipment vanishes during a recession.              The experience I gained there in high speed computer controlled measurement       positioned me well when the increasing speed of analog to digital converters       made digital radio practical. By then I had a stronger background in       computer hardware design than the radio engineers.              The designer of the Japanese Zero fighter couldn't achieve the specified       performance without reducing the strength margin to 1.5x the expected load       to save weight, and others followed. The pilots were ordered not to dive       faster than 350 kts because the lightly built wings would fail at higher       speed. He knew because a diving plane had ripped apart and killed the test       pilot while he was watching. Improving high speed performance would have       added weight and cost some low speed maneuverability, which the authorities       considered more important to win a dogfight. British pilots learned the hard       way that even a Spitfire couldn't dogfight a Zero, though they were       vulnerable at high speed. I read that an F-15 can sometimes outmaneuver an       F-16 because the computer controlled F-16 has an angle of attack limiter       while the F-15 doesn't, and can be pushed closer to a stall. The pilot is       expected to handle the danger.              --- SoupGate-DOS v1.05        * Origin: you cannot sedate... all the things you hate (1:229/2)    |
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