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To: snippy_about_it; SAMWolf; *all
Good morning snippy, SAM, everyone.
7 posted on 05/12/2003 5:05:00 AM PDT by Soaring Feather
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To: bentfeather
Good Morning Feather.
11 posted on 05/12/2003 5:50:00 AM PDT by SAMWolf ((A)bort (R)etry (I)gnore?... Tried Ignore, still have the error.)
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To: *all

Air Power
MiG-31 FOXHOUND

The Mig-31 Foxhound is a substantially improved derivative of the Mig-25 Foxbat. The Mig-31 is an all weather, two seater interceptor with advanced digital avionics. The MiG-31 is a two-seat supersonic (Vmax=3,000 km/h) aircraft with a tapered moderate-swept wings, all-swept twin-fin tail unit and all-moving tailplane. The MiG-31 airframe is an all-metal monoplane with lateral air intakes. Provision is made for installation of two underwing fuel tanks with a total capacity of 5,000 liters.

The most capable Russian air defense interceptor aircraft, the FOXHOUND has a multiple-target engagement capability and was the first Soviet fighter to have a true look-down, shoot-down capability. The N007 Zaslon radar was the first electronically scanned phased array radar to enter service in the world. It could scan 200 km forward and track 10 targets simultanieously. This radar could also track and engage target flying behind and below the aircraft. The Zaslon antenna is of the fixed type, instead of being mechanically directed the radar beam is moved electronically. This allows the full fuselage diameter to be used for the antenna, a considerable advantage since antenna diameter and effective operating range are directly related. Electronic steering of the radar beam is faster than can be performed mechanically, and it is also more accurate. All signal processing is digital.

The radar ensures simultaneous search and attack of several targets using long-range missiles and makes possible to interact within a group. The MiG-31 interceptor fighter can intercept air targets in VFR and IFR weather conditions, day and night and in continuous and discontinuous field of control and guidance commands (solo and in group), of regardless target defensive maneuvers and ECM.

The aircraft avionics enables the use of missiles with radar- and IR-homing heads. The FOXHOUND carries the long-range AA-9 air-to-air missiles, and can engage 4 different targets simultaneouly with the M-9.The MiG-31 aircraft weapons mix comprises four R-33, four R-60M and two R-40T missiles and a GSh-6-23 built-in gun.

The airframe was extensively redesigned for supersonice flight at low altitude, with the welded nickel steel content reduced from the Mig-25's 80% to 49%, with 16% titanium, 33% aluminium alloy and 2% composites. The wings of the aircraft are high-mounted and swept-back with square tips and a negative slant. There are four underwing pylons. There are two turbofan engines in the fuselage. The aircraft is powered by two D-30F6 turbofans developing a takeoff thrust of 15,500 kgf each. The mixed-flow turbofan is fitted with an afterburner and fully-variable flapped jet nozzle. The new Soloviev D-30F6 engine was specified for the MiG-31 in order to improve range, the key performance parameter for which an improvement over the MiG-25 was demanded. There are rectangular and diagonal cut air intakes on sides of the fuselage. The exhausts extend beyond the tail plane. The fuselage is rectangular from the intakes to the exhausts and has a long, pointed nose. The aircraft has a bubble canopy. The tail fins are back-tapered with angular tips and canted outward. The flats are swept-back and tapered and mid- to low-mounted on the body.

The first Mig-31 flew in 1975. By 1987 over 150 FOXHOUNDs were operationally deployed at several locations from the Arkhangelsk area in the northwestern USSR to the Soviet Far East. The FOXHOUND is dedicated to the homeland air defense mission.

In 1992 the Chinese reached agreement with the Russian Federation to buy 24 MiG-31 Foxhound long-range interceptors. The MiG-31s were expected to be assembled at a newly set-up factory in Shenyang, with production at a rate of four per month expected by 2000. The last aircraft was to be delivered by the year 2000. According to some reports the agreement included a license to build as many as 700 aircraft, and some projection envisioned that at least 200 would actually be deployed by the year 2010.

The Mig-31M is an improved version of the basic Mig-31. The key to the MiG-31M's effectiveness is the SBI-16 Zaslon fixed phased array antenna radar, codenamed 'Flash Dance' by NATO, which is said to be the world's most powerful fighter radar. The cockpits were upgraded in the Mig 31M with a number of Cathode Ray Tubes (CRT) and an increased number of missiles.

The MiG-31E provides facilities for vectoring up to three fighters, types MiG-21-93, MiG-23, MiG-25, MiG-29, Su-27 to ensure a covert attack. A group of four MiG-31E fighter-interceptors is capable of interchanging data in the automatic mode on presence of air targets in the zone up to 800 km wide.

The first stage of tests of the upgraded MiG-31BM high-speed multifunctional long-range jet fighter were completed in mid-1999. The main difference between the MiG-31P (Foxhound, according to the NATO classification) and the new MiG-31BM multifunctional air strike system is that the latter is capable of destroying both air and ground targets. The designers and manufacturers of the MiG-31 hope that the new modification will result in international sales. The upgraded MiG-31BM is fitted with a powerful onboard computer system and a radar with a phased array which will allow the pilot to simultaneously activate the air-to-air and air-to-surface missile fire modes. When working with air targets, the MiG-31BM is capable of intercepting up to 24 targets simultaneously.

Specifications:
Countries of Origin: CIS (formerly USSR)
Similar Aircraft: MiG-25 Foxbat, F-14 Tomcat, F-15 Eagle

Crew: Two
Role: Interceptor, air superiority

Dimensions:
Length 70 ft, 5 in (21.5 m)
Span 45 ft, 9 in (14 m)
Height: 6.60 m
Wing span: 14.02 m
Wing area: 61.41 sq m
Weight: (empty) 22,000 kg
Weight: (normal) 36,720 kg

Performance:
Maximum speed: Mach 2.83
Weight: (empty) 22,000 kg
Weight: (normal) 36,720 kg
Powerplant: Two Tumanski R-15BD-300 afterburning turbojets rated at 49.78kN each
Maximum Range: 1,250 km
Service ceiling: 20,700 m
Rate of climb: 8 min 54 sec to 20,000 m
Ceiling: 24400 meters
Cruise range: 1620 nm

In-Flight Refueling: No
Internal Fuel: 14200kg
Drop Tanks: 2000L drop tank with 1600kg of fuel for 91 nm range
Sensors: LD/SD TWS radar, possible IRST, RWR

Armaments:
Cannon
R-33 AA-9 Amos
AA-11 Archer
Typical: two R-40 missiles and Four R-60 missiles




All photos Copyright of Global Security.Org

19 posted on 05/12/2003 7:23:32 AM PDT by Johnny Gage (We will not tire, We will not falter, We will not fail. - George W. Bush)
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To: bentfeather; Pippin
Good afternoon pippin and bentfeather.
21 posted on 05/12/2003 9:03:35 AM PDT by snippy_about_it (Pray for our Troops)
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