NASA NTRS · 19720047257
Propellant flow rate through simulated liquid-core nuclear rocket fuel bed.
Abstract
Experimental investigation of the validity of Zuber and Finlay's (1965) gas flow-rate formula for a two-phase flow in a rotating cylinder under high centrifugal acceleration. This formula was originally derived from tests in a 1-g environment in pipes. In the light of the investigation results obtained, the formula is valid also for a high-g environment in the rotating chamber tested.
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Mcguirk, J. P., Park, C.. 1972-05-01. Propellant flow rate through simulated liquid-core nuclear rocket fuel bed.. https://ntrs.nasa.gov/citations/19720047257
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