| Utilising the proven airframe of the Mirage IIIE, Dassault
undertook a thorough-going modernisation of
equipment and systems to produce the Mirage 3 NG
which flew as a prototype on 21 December 1982. Introducing
features intended to endow it with much improved
air combat performance and survivability in air-ground
operations, the Mirage 3 NG (the suffix signifying
Nouvelle Generation) had non-retractable
swept-back foreplanes, or canards, and highly-swept
wing root leading edge extensions. It possessed a fly-by-
wire control system derived from that of the Mirage
2000, provision for in-flight refuelling, a SNECMA Atar
9K-50 turbojet affording a full afterburning thrust of
7200kg, an advanced nav/attack system
and optional forward-looking sensors, such as a modernised
Cyrano IV radar, a laser rangefinder or Agave
dual-role radar. Maximum take-off weight was increased
by comparison with the Mirage IIIE or 5, four
lateral stores stations were introduced on the fuselage,
and performance improvements included (by comparison
with the IIIE) a 20-25% gain in take-off distance,
40% in time to altitude, a 3050m increase in supersonic ceiling, a three-minute
improvement in intercept time and comparably impressive
gains in acceleration, instantaneous turn rate and
combat air patrol time. No production order was placed
for the Mirage 3 NG and only one prototype was tested.
 | A three-view drawing (1683 x 1043) |
WEIGHTS |
Take-off weight | 14700 kg | 32408 lb |
DIMENSIONS |
Wingspan | 8.22 m | 27 ft 12 in |
Length | 15.65 m | 51 ft 4 in |
Height | 4.50 m | 15 ft 9 in |
Wing area | 35.00 m2 | 376.74 sq ft |
PERFORMANCE |
Max. speed | 2125 km/h | 1320 mph |
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