NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Lift/cruise fan V/STOL technology aircraft design definition study. Volume 1: Technology flight vehicle definitionConcept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fans and the other using mechanically driven fans. The turbotip research technology aircraft reflects maximum usage of existing airframe components. The propulsion system consists of three turbotip fans pneumatically interconnected to three gas generators. Thrust modulation is accomplished by use of energy transfer and control system and thrust reduction modulation. This system can also be operated in the two engine/three fan mode. The mechanical RTA is virtually identical to the turbotip RTA with the exceptions that a different propulsion system and aft fuselage/tail are used. Both aircraft meet or exceed all of the mission performance guidelines and reflect a low cost, low risk approach.
Document ID
19770009070
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, W. J.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
November 18, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-151931
MDC-A4551-VOL-1
Report Number: NASA-CR-151931
Report Number: MDC-A4551-VOL-1
Accession Number
77N16013
Funding Number(s)
CONTRACT_GRANT: NAS2-9245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available