Dassault Rafale

· Dassault Aviation · 2 × Snecma M88

Airplanes

Length

15.27 m

Flat Wing Span

10.9 m

Height

5.34 m

Flat Wing Area

45.7 m²

Max Speed

1912 km/h

Max Ceiling

15835 m

Number of Engines

Aircraft Engine

First Flight

1986-07-04

Entry Into service

2001-05-18

Number Built

316

Maximum Take-Off Weight

24.5 t (paragliders: kg)

Total Fuel Capacity

16550

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity
Dassault Rafale	24.5	16550

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)
Eurofighter Typhoon	Eurojet EJ200	15.96	10.95	Compare
HAL TEDBF	General Electric F414	16.3	11.2	Compare
KAI KF-21 Boramae	General Electric F414	16.9	11.2	Compare
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Fairchild BQ-3	Ranger V-770	15.8496	11.2776	Compare

All data (25 fields)

Name: Dassault Rafale
Manufacturer: Dassault Aviation
Description: The Dassault Rafale (, literally meaning "gust of wind", or "burst of fire" in a more military sense) is a French twin-engine, canard delta wing, multirole fighter aircraft designed and built by Dassault Aviation.
ICAO Code: RFAL
First Flight: 1986-07-04
Entry Into service: 2001-05-18
Designer: Dassault Aviation
Length (m): 15.27
Height (m): 5.34
Cockpit Crew: 1
Max Speed (km/h): 1912
Max Ceiling (m): 15835
Rate of Climb (m/s): 304.8
Armament: 1× 30 mm GIAT 30/M791 autocannon with 125 rounds; 14 External hardpoints for Air and Space Force versions (Rafale B/C), 13 for Navy version (Rafale M)
National Origin: France
Number Built: 316
Powerplant Description: 2 × Snecma M88-4e turbofans, 50 kN thrust each
Primary Users: French Air and Space Force, French Navy , Egyptian Air Force , Indian Air Force , See Operators below for others
Status: In service
Wikipedia Article (URL): en.wikipedia.org/wiki/Dassault_Rafale
Flat Wing Span (m): 10.9
Flat Wing Area (m²): 45.7
Wake Category: M
Aircraft Engine: Snecma M88
Number of Engines: 2