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NSEG: A segmented mission analysis program for low and high speed aircraft. Volume 3: Demonstration problemsProgram NSEG is a rapid mission analysis code based on the use of approximate flight path equations of motion. Equation form varies with the segment type, for example, accelerations, climbs, cruises, descents, and decelerations. Realistic and detailed vehicle characteristics are specified in tabular form. In addition to its mission performance calculation capabilities, the code also contains extensive flight envelope performance mapping capabilities. For example, rate-of-climb, turn rates, and energy maneuverability parameter values may be mapped in the Mach-altitude plane. Approximate take off and landing analyses are also performed. At high speeds, centrifugal lift effects are accounted for. Extensive turbojet and ramjet engine scaling procedures are incorporated in the code.
Document ID
19790012830
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hague, D. S.
(Aerophysics Research Corp. Bellevue, WA, United States)
Rozendaal, H. L.
(Aerophysics Research Corp. Bellevue, WA, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1977
Publication Information
Publisher: NASA
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-CR-2809
Report Number: NASA-CR-2809
Accession Number
79N21001
Funding Number(s)
CONTRACT_GRANT: NAS1-13599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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