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MiG-21 (Fishbed) Russian Fighter Aircraft

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Basic Information
Name
MiG-21 (Fishbed) Russian Fighter Aircraft
Designation
Alternate Designation
Equipment Type
Manufacturer
Russia
Date of Introduction
1959
Description

The Mikoyan-Gurevich MiG-21 (Russian: Микоян и Гуревич МиГ-21; NATO reporting name: Fishbed) is a supersonic jet fighter and interceptor aircraft, designed by the Mikoyan-Gurevich Design Bureau in the Soviet Union. Its nicknames include: Balalaika, because its planform resembles the stringed musical instrument of the same name; Ołówek, Polish for "pencil", due to the shape of its fuselage, and; Én bạc, meaning "Silver Swallow", in Vietnamese. Approximately 60 countries over four continents have flown the MiG-21, and it still serves many nations six decades after its maiden flight. It made aviation records, became the most-produced supersonic jet aircraft in aviation history, the most-produced combat aircraft since the Korean War and previously the longest production run of a combat aircraft (now exceeded by both the McDonnell Douglas F-15 Eagle and General Dynamics F-16 Fighting Falcon). It's also one of the earliest examples of planes capable of performing the Cobra maneuver. The MiG-21 was the first successful Soviet aircraft combining fighter and interceptor characteristics in a single aircraft. It was a lightweight fighter, achieving Mach 2 with a relatively low-powered afterburning turbojet, and is thus comparable to the American Lockheed F-104 Starfighter and Northrop F-5 Freedom Fighter and the French Dassault Mirage III. Its basic layout was used for numerous other Soviet designs; delta-winged aircraft included Su-9 interceptor and the fast E-150 prototype from MiG bureau while the mass-produced successful front fighter Su-7 and Mikoyan's I-75 experimental interceptor combined a similar fuselage shape with swept-back wings. However, the characteristic layout with the shock cone and front air intake did not see widespread use outside the USSR and finally proved to have limited development potential, mainly because of the very small space available for the radar. Like many aircraft designed as interceptors, the MiG-21 had a short range. This was exacerbated by the poor placement of the internal fuel tanks ahead of the centre of gravity. As the internal fuel was consumed, the center of gravity would shift rearward beyond acceptable parameters. This had the effect of making the plane statically unstable to the point of being difficult to control, resulting in an endurance of only 45 minutes in clean condition. This can be somewhat countered by carrying fuel in external tanks closer to the center of gravity. The Chinese variants somewhat improved the internal fuel tank layout (also second generation of Soviet variants), and also carry significantly larger external fuel tanks to counter this issue. Additionally, when more than half the fuel was used up, violent maneuvers prevented fuel from flowing into the engine hereby causing it to shut down in flight. This increased the risk of tank implosions (MiG-21 had tanks pressurized with air from the engine's compressor), a problem inherited from the MiG-15, MiG-17 and MiG-19. The short endurance and low fuel capacity of the MiG-21F, PF, PFM, S/SM and M/MF variants—though each had a somewhat greater fuel capacity than its predecessor—led to the development of the MT and SMT variants. These had an increased range of 250 km (155 mi) compared to the MiG-21SM, but at the cost of worsening all other performance figures, such as a lower service ceiling and slower time to altitude. The delta wing, while excellent for a fast-climbing interceptor, meant any form of turning combat led to a rapid loss of speed. However, the light loading of the aircraft could mean that a climb rate of 235 m/s (46,250 ft/min) was possible with a combat-loaded MiG-21bis, not far short of the performance of the later F-16A. Mig-21's Tumansky R-25 jet engine's specialty was the addition of a second fuel pump in the afterburning stage. Activating the ЧР (rus. "чрезвычайный режим" - emergency mode) booster feature allows the engine to develop 97.4 kilonewtons (21,896 lbf) of thrust under 4,000 meters (13,000 ft) of altitude. The limit of operation is 1 minute for dogfight practice and 3 minutes for an actual wartime emergency, as further use causes the engine to overheat. Use of this "diamond regime" provided a massive 97.4 kN of thrust for no more than 3 minutes in actual wartime use. Use of this temporary power gave the MiG-21bis slightly better than 1:1 thrust-to-weight ratio and a climbing rate of 254 meters/second, equaling the F-16's nominal capabilities in close-quarters dogfight. In air combat practice with the MiG-21bis, use of WEP thrust was limited to 1 minute, to spare on the engines' 800 flight hours lifetime, since every second of super-afterburner use counted as several minutes of regular power run due to extreme thermal stress. When WEP was on, the MiG-21bis's R-25 engine produced a huge 5 meter long blowtorch exhaust - the six or seven brightly glowing rhomboid "shock diamonds" visible inside the flames gave the emergency-power setting its "diamond regime" name. Given a skilled pilot and capable missiles, it could give a good account of itself against contemporary fighters. Its G-limits were increased from +7Gs in initial variants to +8.5Gs in the latest variants. It was replaced by the newer variable-geometry MiG-23 and MiG-27 for ground support duties. However, not until the MiG-29 would the Soviet Union ultimately replace the MiG-21 as a maneuvering dogfighter to counter new American air superiority types. The MiG-21 was exported widely and remains in use. The aircraft's simple controls, engine, weapons, and avionics were typical of Soviet-era military designs. The use of a tail with the delta wing aids stability and control at the extremes of the flight envelope, enhancing safety for lower-skilled pilots; this in turn enhanced its marketability in exports to developing countries with limited training programs and restricted pilot pools. While technologically inferior to the more advanced fighters it often faced, low production and maintenance costs made it a favorite of nations buying Eastern Bloc military hardware. Several Russian, Israeli and Romanian firms have begun to offer upgrade packages to MiG-21 operators, designed to bring the aircraft up to a modern standard, with greatly upgraded avionics and armaments.

Air & Air Defense Specifications
Crew 1
Max Speed 2230.0 km/h
Range 1225.0 km
Service Ceiling 19 m
Variants
Note MiG-21 Fishbed-A/Ye-50 MiG-21 Fishbed-B/Ye-6 MiG-21F Fishbed-C MiG-21PF Fishbed-D MiG-21PF Fishbed-E MiG-21FL Fishbed-E MiG-21PFM Fishbed-F MiG-21 Fishbed-G MiG-21R Fishbed-H MiG-21PFMA Fishbed-J MiG-21MF Fishbed-J MiG-21M Fishbed-J MiG-21SMB Fishbed-K MiG-21bis Fishbed-L MiG-21bis Fishbed-N MiG-21-93 Fishbed-N MiG-21-2000 MiG-21 Lancer MiG-21 Bison MiG-21U Mongol-A** MiG-21US Mongol-B MiG-21UM Mongol-B J-7 (Jianjiji-7) Also See: https://en.wikipedia.org/wiki/List_of_Mikoyan-Gurevich_MiG-21_variants
System
Alternate Designation(s) Mikoyan-Gurevich MiG-21
Primary Function / Type Fighter
Manufacturer Russia
In Service 1959-Present
Crew 1 ea
Number of Engines 1 ea
Number of Hard Points 4 ea
Dimensions
Length 15.76 m
Width (Wing Span) 7.5 m
Height 4.1 m
Weight, Empty 5.46 tons
Weight, Maximum Take Off 10.1 tons
Automotive
Engine Name 1 x R-25-300 turbojet
Traction (dry / with afterburning) 40.2 / 67.2 kN
Maximum Range 1,225 km
Maximum Range with external Fuel Tanks 1,470 km
Maximum Speed 2,230 km/h
Cruising Speed 1,000 km/h
Service Ceiling 19 km
Time to Altitude 17,000 m (55,774 ft) in 8 minutes 30 seconds
Fuel 2,885 liters
Gun Weapon System
System
Name 1 × internal 23 mm Gryazev-Shipunov GSh-23L autocannon
Type Autocannon
Caliber 23 mm
Length GSh-23: 1,387 mm (4 ft 7 in) GSh-23L: 1,537 mm (5 ft 1 in)
Barrels 2 ea
Barrel Length 1,000 mm
Weight GSh-23: 49.2 kg (108 lb) GSh-23L: 50 kg (110 lb)
Action Gast principle
Rate of Fire 3,400–3,600 rounds/min
Muzzle Velocity 715 m/s
Ammunition
Type Rifle, Autocannon
Caliber 23 mm
Cartridge 23x115 mm
Basic Load 200 ea
Wing Mounted Weapon Systems
Air-to-Air Missiles AA-12 Adder AA-11 Archer AA-10 Alamo AA-8 Aphid AA-2 Atoll
Air-to-Surface Missiles unguided bombs, rockets AS-17 Krypton AS-12 Kegler AS-9 Kyle KAB-500Kr
Missile System (Option 1)
Name R-77 (AA-12 Adder)
Type Medium-range, active radar homing air-to-air missile.
Basic Load INA
Production history Manufacturer Vympel
In Service 2002-Present
Proliferation The Russian Air Force finally entered the R-77-1 (AA-12B) into service in 2015.[5][6] It was subsequently deployed by Su-35S fighters in Syria on combat air patrols.
Length 3.6 m (R-77), 3.71 m (R-77-1)
DIameter 200 mm
Warhead 22.5 kg HE fragmenting (R-77)
Detonation Mechanism laser proximity fuse
Engine Solid fuel rocket motor (R-77), air-breathing ramjet (R-77-PD)
Wingspan 700 mm
Operational Range 80–100 km (R-77), 110 km (R-77-1) 193 km (R-77M)
Flight Altitude 5-25 km
Speed Mach 4,Mach 5 for K-77PD (RVV-AE-PD)[
Guidance System Inertial with mid-course update and terminal active radar homing/infrared homing (R-77T)
Launch Platforms Mikoyan-Gurevich MiG-21-93/LanceR/Bison, Mikoyan-Gurevich MiG-23, Mikoyan-Gurevich MiG-25, Mikoyan-Gurevich MiG-27, Mikoyan MiG-29, Mikoyan MiG-31, Mikoyan MiG-35, Sukhoi Su-27, Sukhoi Su-30, Sukhoi Su-33, Sukhoi Su-34, Sukhoi Su-35, HAL Tejas, Yakovlev Yak-141, Chengdu J-10
Missile System (Option 2)
Name KH-31 (AS-17 Krypton)
Type Medium-range air-to-surface
Basic Load INA
Manufacturer Tactical Missiles Corporation (Zvezda-Strela before 2002)
In Service 1988-Present
Proliferation INA
Length Mod 1 : 4.700 m (15 ft 5.0 in)[3] Mod 2 (AD/PD) : 5.3 m (17 ft 5 in)
Diameter 360 mm
Weight Kh-31A :610 kg (1,340 lb) Kh-31P :600 kg (1,320 lb)
Warhead HE shaped charge
Detonation Mechanism Impact
Warhead Weight Kh-31A :94 kg (207 lb) Kh-31P :87 kg (192 lb
Engine Solid fuel rocket in initial stage, ramjet for rest of trajectory
Wingspan 914 mm
Propellant kerosene
Operational Range Kh-31A: 25 km–103 km (13.5–55.6 nmi; Kh-31P: up to 110 km (60 nmi; 70 mi)
Speed Kh-31A/P: 2,160–2,520 km/h (1,340–1,570 mph) MA-31: Mach 2.7 (low), Mach 3.5 (high)
Guidance System Kh-31A: inertial guidance with active radar homing Kh-31P: inertial with passive radar
Launch Platform Both : Su-27SM, Su-30MKI, Su-25, Su-34, Su-35, MiG-29M, HAL Tejas Mk1 and Mk2, MiG-29K Kh-31A only : Su-33 Also : Su-24M
Bomb
Name KAB-500Kr
Type Electro-optical TV-guided fire and forget bomb
Basic Load INA
Manufacturer Russia
Proliferation INA
Length 3.05 m
Diameter INA
Warhead Type Hardened, armor-piercing warhead
Weight 520 kg
Warhead Weight 380 kg
Penetration up to 1.5 metres (4 feet 11 inches) of reinforced concrete.
Effective Range he weapon's seeker can lock onto a target at ranges of up to 15 to 17 km (9.3 to 10.6 mi), depending on visibility.
Note It uses a standard Soviet/Russian FAB-500 general-purpose bomb, with a nominal weight of 500 kg (1,100 lb), as a warhead, adding a low-light television seeker and guidance fins to turn it into a guided, unpowered glide bomb.
Fire Control / Avionics
Fire Control System Type INA
Fire Control Radar Phazotron Kopyo
Laser Desingator INA
Radar Warning Sirena
Protection
Stealth Properties No
Heat Signature Reduction INA
Add on Armor No
NBC Protection Yes
EW Counter Measures INA
Chaffs/Flares BVP-1F 120 x 26-mm cartridge dispenser
Details
Country of Origin Russia
Category Fixed Wing Aircraft
Air > Fixed Wing Aircraft
Filter Label
M
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
15.76 m
Width
7.5 m
Height
4.1 m
Weight
10100 kg
Operators (19)
India
North Korea
Serbia
Angola
Azerbaijan
Croatia
Cuba
Egypt
Guinea
Guinea-Bissau
Libya
Mali
Mozambique
Romania
Sudan
Syria
Uganda
Yemen
Zambia
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