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Grumman X-29
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==Specifications (X-29)== [[File:Grumman X-29 outline.svg|right|350px]] {{Aircraft specs |ref=Jane's All the World's Aircraft 1988-89,<ref name=JAWA88-89>{{cite book |title=Jane's All the World's Aircraft 1988-89 |year=1988 |publisher=Jane's Information Group |location=London |isbn=0-7106-0867-5 |editor1-last=Taylor |editor1-first=John W.R. |edition=79th |pages=399β400}}</ref> NASA X-Planes,{{sfn|Jenkins|Landis|Miller|2003|p=37}} Donald,{{sfn|Donald|1997|p=483}} Winchester{{sfn|Winchester|2005|p=262}} |prime units?=kts <!-- General characteristics --> |crew=1 |capacity={{cvt|4000|lb|0}} payload |length ft=53 |length in=11.25 |length note=including nose probe ::::{{cvt|48|ft|1|in|0}} fuselage only |span ft=27 |span in=2.5 |span note= |height ft=14 |height in=3.5 |height note= |wing area sqft=188.84 |wing area note= |aspect ratio=3.9 |airfoil='''root:''' Grumman K MOD 2 (6.2%); '''tip:''' Grumman K MOD 2 (4.9%)<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |access-date=16 April 2019}}</ref> |empty weight lb=13800 |empty weight note= |gross weight lb= |gross weight note= |max takeoff weight lb=17800 |max takeoff weight note= |fuel capacity={{cvt|3978|lb|0}} in two fuselage bladder tanks and two strake integral tanks |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name= [[General Electric F404-GE-400]] |eng1 type=[[afterburning turbofan]] engine |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |eng1 lbf-ab=16000 <!-- Performance --> |max speed kts=956 |max speed note=at {{cvt|33000|ft|0}} |max speed mach=1.6 |cruise speed kts= |cruise speed note= |stall speed kts= |stall speed note= |never exceed speed kts= |never exceed speed note= |range nmi=350 |range note= |ferry range nmi= |ferry range note= |endurance=<!-- if range unknown --> |ceiling ft=55000 |ceiling note= |g limits=<!-- aerobatic --> |roll rate= |climb rate ftmin= |climb rate note= |time to altitude= |lift to drag= |wing loading lb/sqft= |wing loading note= |fuel consumption lb/mi= |thrust/weight= |more performance=<!--<br /> *'''Take-off run:''' {{cvt||ft|0}} *'''Take-off distance to {{cvt|50|ft|0}}:''' {{cvt||ft|0}} *'''Landing run:''' {{cvt||ft|0}} *'''Landing distance from {{cvt|50|ft|0}}:''' {{cvt||ft|0}}--> |avionics= * Litton LR-80 AHRS * Magnavox AN/ARC-164 UHF * Teledyne RT-1063B/APX-101V IFF/SIF * Honeywell triple redundant fly-by-wire FCS }}
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