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Flight determined acceleration and climb performance of an F-104G airplane for use in an optimum flight path computer programComputer program for optimum flight path defined by flight test investigation of performance characteristics /excess thrust, fuel flow, and climb potential/ of F-104G aircraft
Document ID
19710017526
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Marshall, R. T. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1971
Subject Category
Aircraft
Report/Patent Number
H-636
NASA-TN-D-6398
Report Number: H-636
Report Number: NASA-TN-D-6398
Accession Number
71N27002
Funding Number(s)
CONTRACT_GRANT: 125-17-04-04-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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