 McDonell-Duglass |
VTOL Experimental Aircraft Length : 9.15m
Rotor Diameter : 7.93m Hight : 3.26m Engine : Continental R975-19 (550hp) X 1 Crew : 2 |
 |
VTOL Experimental Aircraft Length : 13.91m
Wing Span : 5.94m Hight : 3.88m Engine : Armstrong Siddeley Mamba II X 1 or Allison 501-C1 X 1 Crew : 1 |
 NASA |
VTOL Experimental Aircraft Length : 9.24m
Width : 9.55m (without Rotor) 16.6m (with Triple-Brade Rotors) Hight : 4.04m Engine : Plat & Whittney R985-AN-1 (450hp) X 1 Max Speed : 296Km/h Range : 400Km Service Ceiling : 4,570m Crew : 2 |
 |
S/VTOL Experimental Aircraft Length : 10.34m
Wing Span : 7.91m Hight : 3.58m All-Up Weight : 5,265Kg Engine : General Electric J85-GE-19 (1,368Kg) X 6 Crew : 1 |
 NASA |
S/VTOL Experimental Aircraft Length : 13.56m
Wing Span : 9.09m Hight : 4.50m All-Up Weight : 5,580Kg Engine : General Electric J85-GE-5 (1,205Kg) X 2 Max Speed : 880Km/h Range : 1,160Km Service Ceiling : 12,200m Crew : 1 |
 NASA |
STOL Experimental Vehicle Length : 5.94m
Wing Span : 10.18m Engine : Continental IO-360-A (210hp) X 1 Max Speed : 105Km/h Crew : 1 |
 McDonell-Duglass |
Hot Cycle Research Aircraft Length : 13.72m
Rotor Diameter : 16.76m Hight : 3.66m All-Up Weight : 6,940Kg Engine : General Electric YT64-GE-6 (2,850hp) X 2 Max Speed : 278Km/h Crew : 2 |
 NASA |
Bell XV-15 Span : 10.72m Hight : 4.67m All-Up Weight : 6,800Kg Engine : Lycoming LTCIK-4K (1,550shp) X 2 Max Speed : 600Km/h Range : 800Km Service Ceiling : 8,8400m Crew : 2 |
