Editing Mikoyan-Gurevich MiG-21 (section)

==Specifications (MiG-21bis)==
{{Aircraft specs
|ref=''Jane's all the world's aircraft, 1992–93'' <ref name=JAWA92-93>{{cite book |title=Jane's all the world's aircraft, 1992–93 |date=1992 |editor1-last=Lambert |editor1-first=Mark |editor2-last=Munson |editor2-first=Kenneth |editor3-last=Taylor |editor3-first=Michael J.H. |publisher=Jane's Information Group |location=Coulson, Surrey, UK |isbn=978-0-7106-0987-8 |edition=83rd|pages=214–216}}</ref>
|prime units?=met
<!--
        General characteristics
-->
|crew=1
|length m=14.7
|length note=excluding pitot boom
|span m=7.154
|span note=
|height m=4.1
|height note=
|wing area sqm=23
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil='''root:''' TsAGI S-12 (4.2%); '''tip:''' TsAGI S-12 (5%)<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 kg=
|empty weight note=
|gross weight kg=8725
|gross weight note=with two [[R-3S]] missiles
|max takeoff weight kg=8800
|max takeoff weight note=unprepared or metal planking runway
::::{{cvt|9800|kg|0}} paved runway with standard wheels and tyres
::::{{cvt|10400|kg|0}} paved runway with larger wheels and tyres
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=1
|eng1 name=[[Tumansky R-25-300]]
|eng1 type=afterburning turbojet
|eng1 kn=40.18
|eng1 note=
|eng1 kn-ab=69.58
<!--
        Performance
-->
|max speed kmh=2175
|max speed note= / M2.05 at {{cvt|13000|m|ft}}
::::{{cvt|1300|km/h|mph kn}} / M1.06 at sea level
* '''Landing speed:''' {{cvt|250|km/h|mph kn}}
|max speed mach=<!-- supersonic aircraft -->
|cruise speed kmh=
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|range km=660
|range note=clean at {{cvt|11000|m}}
::::{{cvt|604|km|mi nmi}} at {{cvt|11000|m}} with two [[R-3S]] missiles
::::{{cvt|793|km|mi nmi}} at {{cvt|10000|m}} with two [[R-3S]] missiles and {{cvt|800|L|USgal impgal}} [[drop-tank]]
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=17500
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate note=
|time to altitude={{cvt|17000|m}} in 8 minutes 30 seconds
|wing loading kg/m2=
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|thrust/weight= 0.76

|more performance=
* '''Take-off run:''' {{cvt|830|m}}
* '''Landing run with SPS and brake parachute:''' {{cvt|550|m}}
<!--
        Armament
-->
|guns=1 × internal [[23×115mm|23 mm]] [[Gryazev-Shipunov GSh-23]]L [[autocannon]] with 200 rounds
|hardpoints=5 (4 underwing + 1 ventral, reserved for fuel droptanks)
|hardpoint capacity=
|hardpoint bombs= 2 × 500 kg (1,100 lb) and 2 × 250 kg bombs
|hardpoint rockets=4 × [[S-24 rocket|S-24]] ''or'' 4× [[UB-16 (rocket pod)|UB-16-57]] rocket pods (4×16 57mm rockets)
|hardpoint missiles=&nbsp;
::*[[Air-to-air missile]]s:
::** [[K-13 (missile)|K-13]]
::** [[K-5 (missile)|R-55]]
::** [[R-60 (missile)|R-60]]
|avionics=
}}