Quote:The Foxbat can *reach* Mach 2.8 for short bursts and cannot be refueled mid-air, the Blackbird cruises at Mach 3.2-3.3 for hours and can be refueled while in flight.
Mach 2.8 sprints only, 777 mile maximum range- does have refuel provisions and nice radar.
Advantage... Blackbird.
Nope the Foxhound has a max speed of Mach 2.83 and the Foxbat A has a max speed of Mach 3+
Here's my proof:
http://www.bharat-rakshak.com/IAF/Aircraft/Specs/MiG-25.htmlOrigin: Russia.
NATO Codename: Foxbat.
Indian Name: Garuda (Mythological Eagle King).
Type: All weather, high-speed reconnaissance aircraft.
Current versions in IAF service: MiG-25R; Single-seat, high-speed reconnaissance.
..........................................MiG-25U; Dual-seat, used for conversion training.
Design Features: The MiG-25U trainer, which had first flown in 1973 and entered service soon after, differed from the single-seat MiG-25 variants in having a totally redesigned forward fuselage component containing two separate cockpits. This trainer version has no SLAR (side-looking airborne radar) nor any reconnaissance capability and is solely used for conversion training.
Accommodation: Pilot on zero/zero ejection seat in A/C and pressurized cockpit.
Avionics: The MiG-25R is equipped with a number of electromagnetic-spectrum sensors along with a larger and a more capable side-looking airborne radar (SLAR). It is fitted with two left-to-right rotating cameras of a focal length of 650mm and 1300mm that can be fitted in the three interchangeable camera bays located in the nose cone of the aircraft.
The two cameras shoot through two port and two starboard windows, and a vertical camera with a shorter focal length is located under the cockpit to make the horizon to horizon linking shots.
Armament: Can carry short & medium range air-to-air missiles for self protection.
Engine: Two Tumansky R-15BD-300 engines each rated at 10,210 kg. of max. thrust.
Maximum Speed: Mach 3+
Service Ceiling: 70,000+ feet
G limit: ?
Maximum Range: ?
Self Defence: ?
Comments: With an inventory of 10 MiG-25R and 2 MiG-25U, they form the No.102 Trisonics Squadron at Bareilly AFB. An indigenous life extension on the MiG-25 is being studied and reportedly the IAF has received preliminary good results.
But the Mig-25 PDS goes Mach 2.83
Specification MiG-25PDS
Type: Single-seat interceptor, reconnaissance aircraft and two-seat conversion aircraft
Power-plant: 2 × Soyuz/Tumansky R15BD-300 turbojet
Power: 86.3 kN (19,400 lb st) dry, 109.75 kN (24,675 lb st) with afterburner
Dimensions: Length: 23.82 m (78 ft 1 3/4 ins)
Span: 14.015 (45 ft 11 3/4 ins)
Height: 6.10 m (20 ft 0 1/4 ins)
Weight: Maximum take-off: 36,720 kg (80,950 lb)
Maximum Speed: Mach 2.83 at altitude
Range: 1,250 km (777 miles)
Armament: Four external attachment points for R-40R (AA-6 'Acrid'), R-40T (AA-6 'Acrid'), R-60, R-23 (AA-7 'Apex'), R-73A (AA-11 'Archer') or R-60T (AA-8 'Aphid') AAMs
here the source:
http://www.soviet-empire.com/arsenal/air/fighters/mig25.phpHere is a list of all type Foxbat based planes:
# MiG-25P Foxbat A
# MiG-25RB Foxbat B
# MiG-25RBV Foxbat B
# MiG-25BBT Foxbat B
# MiG-25R Foxbat B
# MiG-25PU Foxbat C
# MiG-25RU Foxbat C
# MiG-25U Foxbat C
# MiG-25RBK Foxbat D
# MiG-25RBS Foxbat D
# MiG-25RBSh Foxbat D
# MiG-25RBF Foxbat D
# MiG-25PD Foxbat E
# MiG-25PDS Foxbat E
# MiG-25BM Foxbat F
and the solution to the Blackbird has been found:
AA-6 ACRID R-40 In early 1962 the Bisnovat design team began working on the R-40 (K-40), a new long-range missile intended for use with the the MiG-25-40 high- altitude interception system, consisting of the MiG-25 aircraft with Smerch-A radar set and the R-40 missile. Though only slightly larger than the predecessor R-4, the range of the R-40 is over three times greater. This missile was produced in two variants: R-40R (Object RD46 with PARG-12 head) and R-40T (Object TG-46).
After the defection of a MiG-25P to Japan on 06 September 1976, an extensive redesign of the aircraft was undertaken, resulting in the MiG-25PD interception system. Instead of the Smerch-A, a Sapfir-25 radar was installed. The new missile R-40D and its R-40D1 update ("dorabotanaya" [more elaborate]) were produced in two variants R-40RD and R-40TD, both featuring improved countermeasures resistance and a more sensitive homing head to improve performance against low-flying targets. The R-40D1 missile was developed by the Vympel team, the Molniya team having by that time withdraw from development of aircraft missiles. The R-40 is still included among the weapons of MiG-25 and MiG-31 aircraft, although production was discontinued in 1991.
AA-6 ACRID R-40 tech specsManafacturer Bisnovat design team
Date Deployed Late 60s
Range 30 km (R-40) 50 km (R-40TD and R-40RD)
Speed Mach 4.5
Propulsion One solid-propellant rocket motor
Fuze Radar and active laser
Guidance Command, inertial and semi-active radar (R-40R) Command, inertial and IR (R-40T)
Warhead 70 kg HE fragmentation
Launch Weight 475 kg
Length 6.2 m
Diameter 355 mm
Fin Span 1.8 m
Platforms Su-15, MiG-25, MiG-31
hehe this baby goes Mach 4.5