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V/STOL tilt-rotor study, task 1. Volume 1: Conceptual designA conceptual design study was conducted to define a representative military and/or commercial tilt-propeller aircraft for short takeoff and landing operation. The level of structural technology selected for the operational aircraft was based on aluminum, steel, titanium, and adhesive bonded structures. The data describe the following: (1) aircraft weight, (2) performance and stability, (3) aerodynamic noise, (4) dynamic characteristics, (5) maintainability and reliability, and (6) operating economics.
Document ID
19730013199
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Aircraft
Report/Patent Number
REPT-300-099-005-VOL-1
NASA-CR-114441
Report Number: REPT-300-099-005-VOL-1
Report Number: NASA-CR-114441
Accession Number
73N21926
Funding Number(s)
CONTRACT_GRANT: NAS2-6599
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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