Apr 132010
Obviously a stable mate of this concept. A somewhat simplistic design for a two-stage booster utilizing a conventional hydrogen/oxygen first stage (recoverable) with a spherical second stage. The second stage was to be powered by a single terribly powerful gas-core nuclear thermal rocket.
More on this engine & stage in the next APR…
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Sigh.
[…] to this concept, but with a more conventional (but slightly smaller) first stage and a slightly larger second […]