Grumman X-29: Perbezaan antara semakan

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|Pengguna pimary = [[Defense Advanced Research Projects Agency|DARPA]]
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'''[[Grumman]] X-29''' ialah sebuah [[pesawat pejuang eksperimen]] eksperimen milik [[DARPA]] yang ,emgujimenguji beberapa teknologi baru;, terutamanya sayap sapu menghala ke depan danpermukaandan kawalan sayap [[kanard]]. X-29 pertama kali terbang pada 1984 dan dua buah prototaip pesawat X-29 telah diuji terbang dalam dekad berikutnya.
 
==Spesifikasi (X-29)==
{{aero-specs}}
[[Image:Grumman X-29 afg-041110-052.jpg|right|300px]]
{{aircraft specifications
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
|plane or copter?=plane
|jet or prop?=jet
|ref=NASA X-Planes<ref>Jenkins, Dennis R., Tony Landis, and Jay Miller. [http://history.nasa.gov/monograph31.pdf SP-2003-4531, "American X-Vehicles, An Inventory—X-1 to X-50"]. NASA, June 2003.</ref> NASA/Dryden,<ref>[http://www.nasa.gov/centers/dryden/news/FactSheets/Popups/FS-008-DFRC_popup6.html X-29 3-view]. NASA/Dryden Flight Research Center.</ref> Donald,<ref name="World Aircraft"/> Winchester<ref name="Winchester">Winchester, Jim. "Grumman X-29". ''X-Planes and Prototypes''. London: Amber Books Ltd., 2005. ISBN 1-904687-40-7.</ref>
|crew=1
|capacity=
|payload main=4,000 lb
|payload alt=1,810 kg
|length main=48 kaki 1 in
|length alt=14.7 m
|span main=27 kaki 2 in
|span alt=8.29 m
|height main=14 kaki 9 in
|height alt=4.26 m
|area main= 188.8 kaki²
|area alt= 17.54 m²
|airfoil=
|empty weight main= 13,800 lb
|empty weight alt= 6,260 kg
|loaded weight main=
|loaded weight alt=
|useful load main=
|useful load alt=
|max takeoff weight main=17,800 lb
|max takeoff weight alt= 8,070 kg
|more general=
 
|engine (jet)=[[General Electric]] [[General Electric F404|F404]]
|type of jet=[[turbin kipas]]
|number of jets=1
|thrust main=16,000 lbf
|thrust alt=71.2 kN
|thrust original=
|afterburning thrust main=
|afterburning thrust alt=
 
|max speed main=Mach 1.8
|max speed alt=1,100 bsj, 1,770 km/j
|cruise speed main=
|cruise speed alt=
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main=
|range alt=
|ceiling main=55,000 kaki
|ceiling alt=16,800 m
|climb rate main=
|climb rate alt=
|loading main=
|loading alt=
|thrust/weight=
|power/mass main=
|power/mass alt=
|more performance=
 
|armament=
|avionics=
}}
 
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