| | Re: Transit Time to Mars
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| (...) Care to expand on these "USAF experiments"? Got links? Steve (25 years ago, 16-Dec-99, to lugnet.off-topic.geek)
| | | | Re: Transit Time to Mars
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| (...) (URL) some information on the subject in question. apparently it is not all that bad even in atm, but 250 K lbs thrust is not all that much when launching large objects, especially from a 15-20K lb + fuel motor. (It's the burn times that are (...) (25 years ago, 16-Dec-99, to lugnet.off-topic.geek)
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