MACHTRES   FIGHTERS

RAFALE

FRANCE

 

 

 

VARIANTS:

Rafale B: Originally planned dual control, two-seat version for French Air Force; weight 350 kg (772 lb) more than Rafale C; 3 to 5 per cent higher cost than Rafale C. Being developed into fully operational variant for either pilot/WSO or single pilot combat capability.

Rafale C: Single-seat combat version for French Air Force. Detailed description applies to Rafale C, except where indicated.

Rafale D: Original configuration from which production versions derived; now `Rafale Discret' (stealthy) generic name for French Air Force versions.

Rafale M: Single-seat carrierborne fighter; navalisation weight penalty, 610 kg (1,345 lb); take-off weight from existing French carrier Foch limited to 16,500 kg (36,376 lb); has 80 per cent structural and equipment commonality with Rafale C, 95 per cent systems commonality. Navy's financial share of French programme cut in 1991 from 25 to 20 per cent.

AVIONICS:

Comms: EAS V/UHF and TRT Saturn UHF radios. TEAM intercom; Sextant Avionique voice activated radio controls and voice alarm warning system. Thomson-CSF/CNI SB 25A IFF. Chelton aerials. Radar: GIE Radar (Thomson-CSF/Dassault Electronique) RBE2 look-down/shoot-down radar, able to track up to eight targets simultaneously, with automatic threat assessment and allocation of priority.

Flight: SOCRAT VOR/ILS; SAGEM Sigma RL90 INS (interface with carrier's navigation on Rafale M); Thomson-CSF NC 12E Tacan; Sigma RL-90 ring-laser gyro INS; Thomson-CSF/CNI AHV 17 radio altimeter and SFIM/Dassault Electronique flight recorder. Sextant Avionique GPS.

Instrumentation: Digital display of fuel, engine, hydraulic, electrical, oxygen and other systems information on collimated eye-level display and two lateral multifunction touch-sensitive colour LCD displays by Sextant. Fourth cockpit screen is head-level tactical navigation/sensor display. Sextant Avionique CTH3022 wide-angle, holographic HUD incorporating Thomson TTD Optronique OTA 1320 CCD camera and recorder. Sextant/Intertechnique Topsight helmet-mounted sight.

Mission: Thomson-TRT/SAT OSF electro-optical sensors. MIDS (Multifunctional Information Distribution System) datalink (equivalent to JTIDS/Link 16). Various reconnaissance, ECM, FLIR and laser designation pods. Self-defence: Spectra radar warning and ECM suite by Thomson-CSF, Dassault Electronique and Matra. Thomson TTD Optronique DAL (Detecteur d'Alerte Laser) system.

POWER PLANT:

Two SNECMA M88-2 augmented turbofans, each rated at 48.7 kN (10,950 lb st) dry and 72.9 kN (16,400 lb st) with afterburning. M88-3 of 87 kN (19,558 lb st) maximum rating in production aircraft. Internal tanks for more than 5,325 litres (1,406 US gallons; 1,171 Imp gallons) of fuel. Fuel system by Lucas Air Equipement and Zenith Aviation; equipment by Intertechnique. One 1,700 litre (449 US gallon; 374 Imp gallon) drop tank on centreline; 2,000 litre (528 US gallon; 440 Imp gallon) drop tank on each inboard underwing pylon; and/or 1,300 litre (343 US gallon; 286 Imp gallon) tank on each centre underwing pylon. Maximum external fuel 6,600 litres (1,742 US gallons; 1,452 Imp gallons). Pressure refuelling in 7 minutes, or 4 minutes for internal tanks only. Fixed (detachable) in-flight refuelling probe on all versions.

ARMAMENT:

One 30 mm Giat DEFA 791B cannon in side of port engine duct. Fourteen Alkan external stores attachments: two on fuselage centreline, two beneath engine intakes, two astride rear fuselage, six under wings and two at wingtips. Forward centreline position deleted on Rafale M. Normal external load 6,000 kg (13,228 lb); maximum permissible, 8,000 kg (17,637 lb). In strike role, one Aerospatiale ASMP standoff nuclear weapon. In the interception role, up to eight Mica AAMs (with IR or active homing) and two underwing fuel tanks; or six Micas and 5,700 litres (1,505 US gallons; 1,254 Imp gallons) of external fuel. In the air-to-ground role, typically sixteen 227 kg (500 lb) bombs, two Micas and two 1,300 litre (343 US gallon; 286 Imp gallon) tanks; or two Apache standoff weapon dispensers, two Micas and 5,700 litres of external fuel; or FLIR pod, Atlis laser designator pod, two 1,000 kg (2,205 lb) laser-guided bombs, two AS.30L laser ASMs, four Micas and single 1,700 litre (449 US gallon; 374 Imp gallon) tank. In the anti-ship role, two Exocet or projected ANS sea-skimming missiles, four Micas and 4,300 litres .

 

 

 

Technical Specifications

 
 Primary Function: Multirole Fighter
 Contractor: Dassault
 Service Date: 2001
 Crew: Single or twin seater
 Powerplant
  Two SNECMA M88-3 turbofans each rated at 19,555 lb (86.98 kN) with afterburning -- Rafale C
 Dimensions
 Length: 50 ft 3 in (15.3 m)
 Wingspan: 35 ft 9 in (10.9 m)
 Height: 17 ft 6 in (5.34 m)
 Weights
 Empty: Rafale C: 10,000 kg (22,047 lb)

Rafale D: 9,060 kg   (19,973 lb)

Rafale M: 9,670 kg  (21,319 lb)

 Maximum Takeoff: 54,013 lb (24500 kg) -- Rafale C
 Performance
 Speed: Maximum level speed at 36,090 ft (11000 m) 1,321 mph (1,147 kt / 2125 km/h) -- Rafale C
 Ceiling: 60,000 ft
 Range: 570 nm 1,055 Km
 Weapons
  1 x Internal 30mm Giat DEFA 791B Cannon
8 x Mica AAMs
AM39 Exocets
Laser-Guided Bombs
AS 30L Laser Guided ASMs
APACHE Standoff Weapon Dispensers
External load of 6000 kg (13,228 lbs) includes ASMP nuclear standoff missile

SOURCE: ANADEF And OTHERS