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Post Info TOPIC: NS personnel on THE SPACE SHOW
Brucie B.

Date:
NS personnel on THE SPACE SHOW


Yup...Sunday, March 13, 2005 program features Terry McNeeley and Bruce Behrhorst of nuclearspace.com. 


view here:


http://thespaceshow.com/newsletter/


 


The Sunday Space Show is live 12-1:30PM Pacific Time.


 


So tune in and give us your best shot.

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larry

Date:

That's cool.  I won't be able to listen live - but I would like to propose a question.  I always listen to the MP3 of the show.


What would it take for a private company to build a NTR Ship? Is a Man STO possible - pratical from an engineering point of view. Engineering cost?


And I'm not interesting in the political dance you would have to do in making it happen.  I have heard enough of that for that last 25 years.


thanks



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Terry

Date:

If you could gain access to NASA's info on past projects such as NERVA, and ignoring any and all political red tape - maybe a few billion dollars would do the trick. I think it would be best used as an upper stage. But again if you could ignore the public opinion then a large HLV isn't out of the question.

If it was the end of the world, just build a super orion colony ship and get out of dodge! I'm certain even then someone would protest the launch.

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10kBq jaro

Date:

how about an indirect NTR ?


that should minimise the number of ruffled feathers.....


Concept :  use electric power from a nuke plant to fire a multi-megawatt laser beam at the belly of a shuttle craft fueled with hydrogen propellant (only), like an NTR.


Launch is by way of maglev or scram-accelerator, from high-altitude launch site. Laser is located a few hundred miles down-range.


Muzzle is aimed near-vertical, to get out of high-density atmosphere as quickly as possible.


Hypersonic-waverider-type vehicle performs aerodynamic turn in upper part of atmosphere, to convert vertical velocity to horizontal, with minimum losses (high L/D design). Laser heating of propellant heat exchanger on belly provides remainder of thrust required for orbital insertion....



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