Back Bell CTR-800
project

Bell CTR-800

This configuration is based on the XV-15 tilt-rotor and could carry eight passengers. It has a pressurized fuselage and uprated 2100shp Rolls-Royce/Turbomeca RTM-322 engines.

A.J.Pelletier "Bell Aircraft since 1935", 1992

*     *     *

Technical data for Bell CTR-800

Wing span: 9.81m, rotor diameter: 7.92m, overall length: 12.65m, take-off weight: 7135kg, cruising speed: 506km/h, range: 1110km

Do you have any comments concerning this aircraft ?

Name   E-mail


All the World's Rotorcraft


Virtual Aircraft Museum


Back AVIATION TOP 100 - www.avitop.com Avitop.com