| First flown on 22 December 1974, and built as an engine
test bed under official contract, the Mirage F1.M53 was
also envisaged as the basis for a contender in the
contest to find a successor for the Lockheed F-104G in
service with Belgium, Denmark, the Netherlands and
Norway. Evolved from the basic Atar 9K-50 turbojet-powered Mirage F1C, the Mirage F1.M53 - referred to
for a brief period as the "F1E", the suffix letter signifying
Exportation and the designation subsequently
being reassigned - was powered by the SNECMA M53
turbofan rated at 5550kg dry and
8500kg with maximum afterburning.
M53 installation involved significant fuselage structural
redesign, and to provide suitability for ground
attack and long-range interdiction tasks in addition to
that of interception, provision was made for multi-role
avionics. By comparison with the F1C, the F1.M53 had
increased fuel capacity, enlarged engine air intakes
and strengthened undercarriage. The nose profile was
revised to provide for the introduction of a rectractable
flight refuelling probe. The installed armament remained
two 30mm cannon and it was proposed to distribute
up to 4000kg of ordnance between
seven external stations. The other contenders for the
multi-national fighter contract were the Saab 37 Viggen
and the General Dynamics F-16. With choice of the
latter as winner of the competition, plans to produce a
second prototype F1.M53 for testing and integration of
systems were discarded.
WEIGHTS |
Take-off weight | 15200 kg | 33510 lb |
Empty weight | 8024 kg | 17690 lb |
DIMENSIONS |
Wingspan | 8.45 m | 28 ft 9 in |
Length | 15.53 m | 51 ft 11 in |
Height | 4.56 m | 15 ft 12 in |
Wing area | 25.00 m2 | 269.10 sq ft |
PERFORMANCE |
Max. speed | 2335 km/h | 1451 mph |
Range | 1200 km | 746 miles |
johnnie.det@gmail.com, 09.01.2022 06:01 What was the climb rate of F1.M53 and if any, improvements in turn rates? Surely all this was not done to merely increase range reply |
Willicox, e-mail, 23.12.2021 23:38 Π'ΡΠ΅ΠΌ ΠΏΡΠΈΠ²Π΅Ρ! reply |
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The inclusion of the Mail would have improved the Mirage F1's performance all-round, including better take off performance in high temperature climates like the Middle East, as well as heavier ordnance /fuel fraction with less lose of flight performance, when compared to the legacy Atar-powered Mirage F1.
Regards
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