Possibilities for thermonuclear reactions to be used as energy source for propulsion of atomic rockets, photon rockets, turbojets, and ram jets; results indicate maximum heat production at 108 K for hydrogen isotopes. English translation from Astronautica Acta pt 2 1955.
Steady nuclear combustion in rockets
NACA -- Tech Memo
1957
39 pages
Article (Journal)
English
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NTIS | 1968
|AIAA | 1967
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