Super-Mirage: Difference between revisions

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<!-- General characteristics -->
<!-- General characteristics -->
|crew=2 (Pilot and Radar Intercept Officer)
|crew=2 (Pilot and Radar Intercept Officer)
|length =
|length main=19.1 m
|length alt=62.66 ft
|span main=11.2 m
|span main=11.2 m
|span alt=36.7 ft
|height main=5.8 m
|height main=5.8 m
|empty weight main=  
|height alt=19 ft
|empty weight main=14,187 kg
|empty weight alt=31,276 lb
|loaded weight main=
|loaded weight main=
|max takeoff weight main=
|max takeoff weight main=29,000 kg
|max takeoff weight alt=63,934 lb
<!-- Powerplant -->
<!-- Powerplant -->
|engine (jet)=
|engine (jet)=M53-P20
|type of jet=
|type of jet=afterburning turbofans
|number of jets=
|number of jets=2
|thrust main=
|thrust main=64.7 kN
|thrust alt=
|thrust alt=14,545 lbf
|afterburning thrust main=
|afterburning thrust main=98,06 kN
|afterburning thrust alt=
|afterburning thrust alt=22,044 lbf
<!-- Performance -->
<!-- Performance -->
|max speed main=<br/>
|max speed main=<br/>
**'''High altitude:'''  
**'''High altitude:''' Mach 2.2
**'''Low altitude:'''  
**'''Low altitude:''' Mach 1.2
|max speed alt=
|max speed alt=
|max speed more=
|max speed more=
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|range alt=
|range alt=
|range more=
|range more=
|combat radius main=
|combat radius main=2,000 km
|combat radius alt=
|combat radius alt=1,242 mi
|combat radius more=
|combat radius more=
|ferry range main=
|ferry range main=5,000 km
|ferry range alt=
|ferry range alt=3,106 mi
|ferry range more=
|ferry range more=
|ceiling main=
|ceiling main=20,000 m
|ceiling alt=
|ceiling alt=65,616 ft
|climb rate main=
|climb rate main=305 m/s
|climb rate alt=
|climb rate alt=60,000 ft/min
|thrust/weight=  
|thrust/weight= 0.9
|more performance=
|more performance=
<!-- Armament -->
<!-- Armament -->

Revision as of 07:21, 14 February 2020

Super-Mirage
ACFtrials.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
Sieuxerrian Navy
Produced 1984–present
Number built 300~
Developed from Mirage-Menace

The Dassault Super-Menace is a twin or single-seat, twinjet, interceptor, air superiority fighter and Strike fighter used by the Sieuxerrian Navy and Sieuxerrian Air Force. Developed from the Mirage-Menace, the Super-Mirage features a matured design, improved sensors, upgrade capacity, and armament. It shares some design features, a common engine, and other similar parts, allowing for relaxed logistical need to maintain the aicraft between the air force and the navy.

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 Radar Intercept 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