NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Propellant flow rate through simulated liquid-core nuclear rocket fuel bed.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.
Document ID
19720047257
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Mcguirk, J. P.
(Santa Clara, University Santa Clara, Calif., United States)
Park, C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 9
Subject Category
Nuclear Engineering
Accession Number
72A30923
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available