Mikoyan-Gurevich 23-01
| {{Infobox aircraft begin
| name=Mikoyan-Gurevich 23-01 | image=File:Mikoyan 23-01.png | caption=a 2-view of the 23-01 }}{{Infobox aircraft type | type=Mikoyan-Gurevich 23-01 | national origin=USSR | manufacturer=OKB Mikoyan-Gurevich | designer=V A Mikoyan (project manager) | first flight=3 April 1967 | introduced= | retired= | status= | primary user= | more users= | produced= | number built= | program cost= | unit cost= | developed from= Mikoyan-Gurevich 23-31 / Izdeliye 92 | variants with their own articles= }} |
The Mikoyan-Gurevich 23-01, aka Izdeliye 92 and (erroneously) Mikoyan-Gurevich MiG-23PD, NATO reporting name Faithless, was a 1960s STOL fighter / attack aircraft, designed in the USSR, to fulfil a requirement for ground-attack and fighter aircraft able to operate from short runways.
Specifications (23-01)
{{Aircraft specs
|ref=Soviet X-Planes{{cite book |last1=Gordon |first1=Yefim |title=Soviet X-Planes |year=2000 |publisher=Midland |location=Hinkley |isbn=978-1-85780-099-9 |last2=Gunston |first2=Bill |pages=118–119}}
|prime units?=met
|crew=1
|length m=16.8
|length ft=
|length in=
|length note= (excl. PVD boom)
|span m=7.72
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=40
|wing area sqft=
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=12020
|empty weight lb=
|empty weight note=
|gross weight kg=16000
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Tumansky R-27-300
|eng1 type=afterburning turbojet engine
|eng1 kn=
|eng1 lbf=
|eng1 note=
|eng1 lbf-ab=17196
|eng2 number=2
|eng2 name=Rybinsk RD-36-35
|eng2 type=turbojet engines
|eng2 lbf=10362
|eng2 note=lift engines for STOL operations only
|perfhide=
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|never exceed speed kmh=
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|never exceed speed kts=
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|range km=
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|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
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|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
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|fuel consumption lb/mi=
|power/mass=
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|more performance=
- Take-off run: {{cvt|180|-|200|m|0}} at light AUW
- Landing run: {{cvt|250|m|0}} with brake parachute
|missiles= displayed with dummy Vympel R-23R and R-23T missiles on two underwing pylons
|avionics=Provision for a large fire-control radar in the nose
}}
References
{{reflist}}
{{Mikoyan aircraft}}
{{Authority control}}
{{DEFAULTSORT:Mikoyan-Gurevich 23-01}}
Category:1950s Soviet fighter aircraft