NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Rocket exhaust plume computer program improvement. Volume 1: Summary: Method of characteristics nozzle and plume programsA summary is presented of the various documents that discuss and describe the computer programs and analysis techniques which are available for rocket nozzle and exhaust plume calculations. The basic method of characteristics program is discussed, along with such auxiliary programs as the plume impingement program, the plot program and the thermochemical properties program.
Document ID
19720011292
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ratliff, A. W. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Smith, S. D. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Penny, N. M. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1972
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-125601
LMSC/HREC-D162220-VOL-1
Report Number: NASA-CR-125601
Report Number: LMSC/HREC-D162220-VOL-1
Accession Number
72N18942
Funding Number(s)
CONTRACT_GRANT: NAS7-761
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available