NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
The prediction of the nonlinear behavior of unstable liquid rocketsAnalytical technique for solving nonlinear combustion problems associated with liquid propellant rocket engines
Document ID
19710025465
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Powell, E. A.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Zinn, B. T.
(Georgia Inst. of Tech. Atlanta, GA, United States)
Date Acquired
August 6, 2013
Publication Date
July 1, 1971
Subject Category
Propellants
Report/Patent Number
NASA-CR-72902
Report Number: NASA-CR-72902
Accession Number
71N34941
Funding Number(s)
CONTRACT_GRANT: NGL-11-002-083
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available