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To: BenLurkin

The whole deal is an embedded systems problem.

Believe me. This is a complicated problem...when they work it out it will shave mucho $$$ from the cost of a space launch.

It is ROCKET SCIENCE after all....


3 posted on 04/19/2015 2:58:49 PM PDT by Bobalu (If we live to see 2017 we will be kissing the ground)
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To: Bobalu
Yep. I was project historian for the National Aerospace Plane program, 1988-1995 (wrote the official history called "The Quest for the Orbital Jet," (http://www.amazon.com/Hypersonic-Revolution-Studies-History-Technology/dp/1478146176/ref=sr_1_2?s=books&ie=UTF8&qid=1429481235&sr=1-2&keywords=ThE+Quest+for+the+orbital+jet)

Anyway, it was amazing to watch the difficulties of solving so many of these problems. One rationale for building the X-30 was that, like Obamacare, to know how to test it we had to build it. There were no wind tunnels for Mach 15-20, so really except for computer models, the only way they could get real data was to build stuff and test it.

8 posted on 04/19/2015 3:07:04 PM PDT by LS ('Castles made of sand, fall in the sea . . . eventually.' Hendrix)
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To: Bobalu

I do not understand how this will save any money. Swapping payload weight for return fuel weight does not help the launch vehicle company make a profit. “We got our first stage back safely but we were not able to put enough payload into orbit to make a profit.” That is why the traditional launch vehicle companies do not try to save their boosters.


28 posted on 04/19/2015 4:56:40 PM PDT by robert14 (cng)
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