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