NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
One-dimensional nonlinear model for determining combustion instability in solid propellant rocket motorsNonlinear analysis of combustion instability in solid propellant rocket engines
Document ID
19660014187
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Povinelli, L. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-3410
Report Number: NASA-TN-D-3410
Accession Number
66N23476
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SOLID PROPELLANT ROCKET ENGINE
COMBUSTION INSTABILITY
No Preview Available