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Converging-diverging nozzle thruster code for nuclear or chemical rocket performance computations /

Bibliographic Details
Main Author: Juhasz, Albert J. (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2019.
Series:NASA technical memorandum ; 2019-220164.
Subjects:
Nozzle thrust coefficients.
Computer programs.
Rocket thrust.
Molecular weight.
Propellant properties.
Online Access:https://purl.fdlp.gov/GPO/gpo121321
Description
Item Description:"April 2019."
Physical Description:1 online resource (18 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 17-18).