View source for Nakajima ATD-X

{{wip}}
{|{{Infobox aircraft begin
|name= ATD-X
|image= File:X-2_First_Flight.jpg
|caption= The ATD-X during its maiden flight.
}}{{Infobox aircraft type
|type= Experimental stealth aircraft
|national origin= {{flag|Chilokver}}
|manufacturer= [[Nakajima Aircraft Company]] 
|status= Retired
|first flight= 
|introduction= 
|primary user= [[National Chilokveri Air Force]]
|more users= 
|produced=
|number built= 1
|program cost= CL₡408.4 million (2016 estimate)
|unit cost=  
|developed from=  
|variants with their own articles= 
}}|}

The '''Nakajima ATD-X''' ('''Advanced Technology Demonstrator – Experimental''') was an experimental [[Chilokver|Chilokveri]] aircraft used to test low-observable airframe shaping, {{wpl|Radiation-absorbent_material|radar-absorbent materials}}, {{wpl|Thrust_vectoring|thrust vectoring}}, and other fifth-generation aircraft technologies. The aircraft was developed by [[Nakajima Aircraft Company]] in collaboration with the [[Chilokveri Ministry of Defence]], and the sole prototype constructed was flown by the [[National Chilokveri Air Force]] (NCAF). The ATD-X's first flight was on November 21, 2014.

==Development==
The ATD-X project began in 2001 as the '''Advanced Combat Aircraft''' (ACA) programme to design, develop, and manufacture a next-generation fighter to replace the [[National Chilokveri Air Force|NCAF'S]] existing fleet of [[Shangtian CF-03 Falcon|CF-03 Falcon]] and [[Nakajima CF-04 Falconet|CF-04 Falconet]] multirole fighters. The initial requirements of the ACA programme, as originally proposed by the NCAF, were to develop a 5th generaton, single-seat, twin-engine fighter with stealth capabilities. In July 2001, the [[Chilokveri Ministry of Defence|Chilokveri Ministry of Defence's]] [[Research and Procurement Agency]] (RPA) awarded [[Nakajima Aircraft Company|Nakajima]] with a ₡24 million [[Chilokveri credit|credit]] contract for the development of a preliminary design.

==Design==

==Specifications==
{{Aircraft specs
|prime units?=met
|crew=1
|capacity=
|length m= 14.17
|length ft=
|length in=
|length note= 
|span m= 9.10
|span ft=
|span in=
|span note=
|height m= 4.51
|height ft=
|height in=
|height note=
|wing area sqm=
|wing area sqft=
|wing area note=
|empty weight kg= 8900
|empty weight lb=
|empty weight note=
|gross weight kg= 
|gross weight lb=
|gross weight note=
|max takeoff weight kg= 13000
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general= 

|eng1 number= 2
|eng1 name= [[Kowasaki TF5]]
|eng1 type= {{wpl|Bypass ratio|low-bypass}} {{wpl|Turbofan|turbofans}}
|eng1 kn= 
|eng1 lbf= 
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab= 11023

|max speed kmh= 
|max speed mph=
|max speed kts= 
|max speed note=
|max speed mach= 2.25 (2,778 km/h; 1,726 mph)
**'''Supercruise:''' Mach 1.82 (2,247 km/h; 1,396 mph)
|cruise speed kmh= 
|cruise speed mph=
|cruise speed kts= 
|cruise speed note= 
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|range km= 2,900
|range miles= 
|range nmi= 1,566
|range note=
|combat range km= 761
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km= 3,200
|ferry range miles= 1,988
|ferry range nmi= 1,728
|ferry range note=
|endurance=
|ceiling ft= 65000
|ceiling m=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|thrust/weight=

|more performance=

|avionics=
}}

==See also==

[[category:Chilokver]]