NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Transonic transport study: EconomicsAn economic analysis was performed to evaluate the impact of advanced materials, increased aerodynamic and structural efficiencies, and cruise speed on advanced transport aircraft designed for cruise Mach numbers of .90, .98, and 1.15. A detailed weight statement was generated by an aircraft synthesis computer program called TRANSYN-TST; these weights were used to estimate the cost to develop and manufacture a fleet of aircraft of each configuration. The direct and indirect operating costs were estimated for each aircraft, and an average return on investment was calculated for various operating conditions. There was very little difference between the operating economics of the aircraft designed for Mach numbers .90 and .98. The Mach number 1.15 aircraft was economically marginal in comparison but showed significant improvements with the application of carbon/epoxy structural material. However, the Mach .90 and Mach .98 aircraft are the most economically attractive vehicles in the study.
Document ID
19720019365
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Smith, C. L.
(NASA Ames Research Center Moffett Field, CA, United States)
Wilcox, D. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62159
Report Number: NASA-TM-X-62159
Accession Number
72N27015
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available