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One-dimensional two-phase reacting gas nonequilibrium performance programComputer program calculates the inviscid one-dimensional equilibrium, frozen, and nonequilibrium nozzle expansion of propellant exhaust mixtures containing carbon, hydrogen, oxygen, nitrogen, fluorine, chlorine and either aluminum, beryllium, boron or lithium. This program performs calculations for conical nozzles only.
Document ID
19680000376
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Cherry, S. S.
Frey, H. M.
Kliegel, J. R.
Quan, V.
Date Acquired
August 4, 2013
Publication Date
October 1, 1968
Subject Category
Mathematics And Information Sciences
Report/Patent Number
MSC-11780
Report Number: MSC-11780
Accession Number
68B10376
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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