Super-Mirage

Revision as of 16:04, 2 September 2022 by SanSilv (talk | contribs)
Jump to navigation Jump to search
Super-Mirage
Dassault Mirage 4000, France AN2164548.jpg
Super-Mirage prototype 001 in the late 1970s.
Role Interceptor, air superiority fighter, Strike fighter
National origin Sieuxerr
Manufacturer Dassault
Designer Dassault
First flight 1977
Introduction 1984
Status In service
Primary user Sieuxerrian Air Force
Solevant Air Force
Produced 1984–present
Number built 300~
Developed from Dassault Mirage 2000

The Dassault Super Mirage (Known also as the Super Mirage 4000 or simply the Mirage 4000)

Design

Overview

Cockpit

Engines

The Super-Mirage is equipped with two Snecma M53 afterburning turbofan engines. Equipped with the improved M53-P2 found in the Mirage-Menace and the Dassault Mirage 2000. From 2005 to 2011, the entire fleet was upgraded with the M88-10 engine, based off the M88-2 engine used by the Rafale, generating 70 kN (15,500 lbf) and 100 kN (25,000 lbf) (with afterburner). The engine greatly improved handling of the aircraft at speed.

Weaponry

The Menace is equipped with a single 30mm GIAT 30 revolver cannon with selectable rate of fire of 300 rpm to 2,500 rpm. It is mounted under the right intake.

Avionics

The Super-Mirage uses a derivative of the Thomson-CSF Giraffe radar from the Menace. It achieves upwards of 165km range against comparable fighter-sized objects with over 270km range against large bomber-sized objects. It has multi-target tracking abilities. In the mid-2000s, apart of a major overhaul, the older mechanically scanned radar arrays were replaced by electronically scanned active radar arrays.

Operational history

Operators

Current

Specifications

MenaceC19823view.png

General characteristics

  • Crew: 2 (Pilot and Weapon Systems Officer)
  • Length: 19.1 m (62.66 ft)
  • Wingspan: 11.2 m (36.7 ft)
  • Height: 5.8 m (19 ft)
  • Empty weight: 14,187 kg (31,276 lb)
  • Max. takeoff weight: 29,000 kg (63,934 lb)
  • Powerplant: 2 × M53-P20 afterburning turbofans
    • Dry thrust: 64.7 kN (14,545 lbf) each
    • Thrust with afterburner: 98,06 kN (22,044 lbf) each

Performance

Armament