US Naval X-Numbers PAGE

2008 / 10 / 26 Update.



Bell Aerosystems
Bell X-22A VTOL Experimental Aircraft
Length : 12.06m
Wing Span (Front) : 7.0m
Wing Span (Rear) : 11.96m
Hight : 6.31m
Wing Area (Front) : 12.91 Square meter
Wing Area (Rear) : 26.57 Square meter
All-Up Weight : 8,172Kg
Empty Weight : 5,197Kg
Engine : General Electric YT58-GE-8D Turbo Shaft (1,050shp) X 4
Max Speed : 410Km/h
Max Altitude : 8,500m
Range : 720Km
Crew : 2

Lockheed-Martin
Lockheed X-26A
Length : 8.15m
Wing Span : 17.4m
Hight : 2.82m
Wing Area : 16.72 Square meter
Empty Weight : 648.6Kg
Engine : unpowered
Max Speed : 254Km/h
Max Altitude : 5,638m
Crew : 2

Lockheed
Lockheed X-26B
Length : 9.42m
Wing Span : 17.4m
Hight : 2.82m
Wing Area : 16.72 Square meter
All-Up Weight : 990Kg
Empty Weight : 715Kg
Engine : Continental O-200-A (100hp) X 1
Max Speed : 185Km/h
Max Altitude : 3,960m
Range : 560Km
C
rew : 2
Pereira Osprey II
( The archetype of X-28 Osprey I )

Lockheed-Martin
Pereira X-28 Ospray
Length : 5.26m
Wing Span : 7.0m
Hight : 1.60m
Empty Weight : 408Kg
Engine : Continental C90-12 X 1
Max Speed : 217Km/h
Max Altitude : 5,486m
Crew : 1

Boeing
Boeing X-46 UCAV-N
Length : 9.75m
Wing Span : 12.19m

Northrop-Grumman

Northrop-Grumman X-47A Pegasus UCAV Experimental Aircraft
( The Prototype of UCAV-N )
Length : 8.5m
Wing Span : 8.5m
Hight : 1.60m
Engine : Plat & Whittney JT15D-5C (1,450Kg) X 1


DAPRA
Northrop-Grumman X-47B UCAV Aircraft
( The Prototype of UCAV-N )


Boeing
Boeing X-50 CRW (Canard Rotor Wing) Experimental Aircraft
Length : 5.39m
Wing Span : 2.71m
Hight : 1.98m
Engine : Turbo Fan X 1
Max Speed : 700km/h