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The AC-120: The advanced commercial transportThe main objective of this design was to fulfill a need for a new airplane to replace the aging 100 to 150 passenger, 1500 nautical mile range aircraft such as the Douglas DC9 and Boeing 737-100 airplanes. After researching the future aircraft market, conducting extensive trade studies, and analysis on different configurations, the AC-120 Advanced Commercial Transport final design was achieved. The AC-120's main design features include the incorporation of a three lifting surface configuration which is powered by two turboprop engines. The AC-120 is an economically sensitive aircraft which meets the new FM Stage Three noise requirements, and has lower NO(x) emissions than current turbofan powered airplanes. The AC-120 also improves on its contemporaries in passenger comfort, manufacturing, and operating cost.
Document ID
19940020484
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Duran, David
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Griffin, Ernest
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Mendoza, Saul
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Nguyen, Son
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Pickett, Tim
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Noernberg, Clemm
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
May 14, 1993
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-195491
NAS 1.26:195491
Report Number: NASA-CR-195491
Report Number: NAS 1.26:195491
Accession Number
94N24966
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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