 Hiller Helicopter |
"Flying Plathome" VTOL Experimental Vehicle Engine : Nelson H-56 Air Cooling Engine X 2 |
 Hiller Helicopter |
VTOL Experimental Vehicle |
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The Prototype of VZ-2 |
 NASA |
Tilt Wing V/STOL Experimental Aircraft Length : 8.05m
Rotor Diameter : 2.90m Width : 7.60m Hight : 3.25m ngine : Lycoming YT53-L-1 (700hp) X 1 Crew : 1 |
 US ARMY |
V/STOL Experimental Aircraft Length : 8.43m
Wing Span : 7.14m Hight : 3.25m All-Up Weight : 1,180Kg Engine : Abco-Lycoming T53-L-1 (1,000shp) X 1 Crew : 1 |
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Ducted Fun VTOL Experimental Aircraft Length : 9.75m
Width : 7.77m Hight : 3.05m All-Up Weight : 1,452Kg Engine : Lycoming YT543 (840shp) X 1 Max Speed : 370Km/h Service Ceiling : 1,830m Range : 370Km Crew : 2 |
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VTOL Experimental Aircraft Length : 10.26m
Hight : 5.13m All-Up Weight : 1,803Kg Engine : General Electric YT58-GE-2 Turboshaft (1,024shp) X 1 Max Speed : 297Km/h Crew : 2 |
 US Army Transportation Corps Museum |
Propella Diameter : 2.59m Hight : 1.57m All-Up Weight : 1,088Kg Engine : Lycoming piston engine (500shp) Crew : 1 |
 US Army Transportation Corps Museum |
Propella Diameter : 1.98m Span : 4.87m Hight : 2.83m All-Up Weight : 952Kg Own weight : 771Kg Engine : Turboméca Artouste II B turboshaft engine (425shp) Max Speed : 51Km/h Cruising Speed : 40Km/h Service Ceiling : 60.9m Armament : None Crew : 1 (the second prototype : 2) |
 US Army Transportation Corps Museum |
Rotor Diameter : 2.26m Width : 2.87m Hight : 2.01m All-Up Weight : 1,065Kg Own weight : 838Kg Engine : Turboméca Artouste II B turboshaft engine (425shp) X 1 Lycoming O-360-A2A piston engine (180shp) X 2 AiResearch TPE331-6 turbine (550shp X 1) Max Speed : 104Km/h Cruising Speed : 80Km/h Service Ceiling : 914m Range : 40Km Crew : 2 |
 Piasecki |
Rotor Diameter : 2.5m Width : 2.81m Hight : 1.77m All-Up Weight : 1,664Kg Own weight : 1,184Kg Engine : Turboméca Artouste II C turbine (400shp) X 2 Max Speed : 136Km/h Cruising Speed : 112Km/h Service Ceiling : 914m Range : 56Km Crew : 2 + 3 |
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Diameter : 5.48m |
