Strange, I thought NASA was the organisation that hit a comet travelling umpteen thousands of miles an hour exactly where they wanted to when they wanted to, as opposed to the military here who can't even hit a missile travelling a few thousand miles an hour right here in their backyard half the time.
When I worked on the spaceborne "black box" data recorder for the Shuttle, one goal was to limit the multi-pin connector (certified for thousands of connect/disconnect cycles) to exactly two connects and two disconnects. Why? Because we could, and it reduces the chance of damage slightly. We did this:
("-->>--" is a connector)
A B C TEST SET-->>-->>-->>--RECORDER
A B C SHUTTLE-->>-->>-->>--RECORDER
By always connecting/disconnecting B, we could almost always limit A and C to two connects and two disconnects.
Remember the Shuttle O-Ring? I was part of the team that made the system that tested them for flaws. Alas, the joint designers allowed the O-Rings to see conditions that were out of spec; our temerature limits did not allow direct contact between the O-ring and the flame from a solid-fuel booster rocket. :(
Now I know who to thank for ordering a redesign of the 17 inch disconnect for the external fuel tank. I made a lot of money on that one. Not that it was wasted, though; the 17" disconnect is one of the places where there is no redundancy - a failure to close will bring down a shuttle.
1) NASA or the contractor spent zillions on testing systems, and they couldn't do a redundant PSU test properly. I hate to think what the other test were like.
2) "fastest space qualification ever" So why did everything else take so long?
On a sunny day (Thu, 14 Jul 2005 19:18:21 +0000) it happened Guy Macon wrote in :
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EDUCATION:
EDUCATION: I am self taught; I started as an assembler and worked my way up to technician, then engineer. I do not have a degree, but I do have over twenty years of experience and a proven record of accomplishment in the area of product development. It shows. You need a shave.
First of all, they knew the path of the comet. Second of all, it tooks years to achieve this. Much harder to do it in say, a half minute window.
Back in the 50's I think it was, the Army claimed they hit the moon with a ball bearing shot from a Redstone Rocket or something to that effect. I don't think there was such a thing as a uP then. toobs, maybe?
On a sunny day (Thu, 14 Jul 2005 19:42:27 GMT) it happened Al wrote in :
There were little metal toobs, 'nuvistor??? ah here:
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But that was end fifties. There were other small tubes too, before the transistor. The name 'nuvistor' sort of looks like it was a last attempt to challenge the first transistors (1958 was it these came?). But of cause mechanical gyroscopes were there long before, also in the V2 in WW2. I have seen nuvistors used only once IIRC, typical application was preamp in a capacitor microphone.... These mikes were big and still around in the sixties.
I am guessing a $1000 redesign will probably take 10 years and millions of dollars to test and certify .... Well it would if you use the software testers I used to work with....
Wouldn't it also have to be specifically space certified, and hence tested against long term radiation exposure? Also, I would have thought that the repeated acceleration (G force) testing of a space certified part would be have to be far more extensive. $250k as a conservative starting point looks about right.
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