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What is involved in 'safing' a shuttle?



 
 
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Old March 1st 10, 01:09 AM posted to sci.space.policy,sci.space.shuttle,sci.space.station
Pat Flannery
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Default What is involved in 'safing' a shuttle?

On 2/28/2010 12:44 PM, Jochem Huhmann wrote:


Well, there are lots of things that aren't exactly impossible from a
physics point of view, but still really complicated. Repeating all the
uncertainties of ignition (and to do this with changing temperatures of
the systems) hundreds of times a second is surely not going to give you
more accuracy, I think.


RC planes are fueled with a nitromethane/methanol mixture, and pure
nitromethane can be used as a monopropellant, just like hydrazine:
http://en.wikipedia.org/wiki/Nitromethane
Simply heating it will cause it to decompose, and it's a lot more benign
to work with than hydrazine.
Another monopropellant is Otto Fuel II, such as is used in torpedoes; it
is mildly toxic:
http://en.wikipedia.org/wiki/Otto_fuel_II

Pat
 




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