PLAY
Aviation
◌Mirage IIIS C.70
VII
Rank
AB
10.3
RB
10.3
SB
10.3
Battle rating
Germany
Research country
Fighter
Main role
260,000
RP
Research
710,000
SL
Purchase
Switzerland
Operator
General information

The Mirage IIIS C.70 is an upgraded version of the Mirage IIIC fighter jet, developed in Switzerland. At the time, Switzerland had a decent air force that included various subsonic fighter jets. However, the lack of a supersonic aircraft was a significant drawback. Therefore, the Air Force created a program to introduce a new fighter jet. Participants included the Saab 35, the G.91, the F-104, the Mirage IIIC, and the F-11F-1F. Ultimately, the Mirage IIIC was selected. In 1961, Switzerland purchased one Mirage IIIC aircraft. Subsequently, production was localized, and the aircraft was renamed the Mirage IIIS. The military planned to build 100 of these fighters, but the necessary funding was not allocated. Consequently, only 54 aircraft were built, 16 of which were Mirage IIIRS reconnaissance variants. The Mirage IIIS entered combat duty in 1967.

Work on improving the Mirage IIIS began in 1988. The most notable improvement was the addition of canards, which enhanced stability during takeoff and landing and increased maneuverability. The name of this modification, C.70, comes from "Canard Wing at 70%". The new fighter was also equipped with updated avionics. Most Mirage IIIS C.70s were decommissioned at the Mirage-99 ceremony in 1999. But a few remained in service until 2003.

The Swiss Mirage IIIS C.70 was introduced in Update 2.47 "Leviathans", as a part of the German aviation research tree. Compared to its French predecessor, the aircraft has updated avionics and can use SARH AIM-26 missiles. As for IR missiles, the aircraft has a licensed copy of the AIM-9E. The Mirage IIIS C.70 can also use the SEPR844 booster with its standard armament and new JATO rocket boosters. Disadvantages of the aircraft include high speed loss during maneuvers and the lack of any air-to-ground weapons.



Flight performance
Max speed
at 12,000 m 2,1602,0592,2262,095 km/h
Rate of Climb 14098.7173.3109 m/s
Turn time 2830.426.429.7 s
Max altitude 16,000 m
Takeoff Run 750 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 14.8 m
Wingspan 8.2 m
Wing Loading 262 kg/m²

Weight:
Base weight 7.137.366.947.32 t
Fuel in main tanks 1.9 t (28m)
Fuel in drop tanks 1.02 t (15m)
Fuel for additional engines 1.32 t

Limits:
Max Speed Limit (IAS) 1,460 km/h
Mach Number Limit 2.1 M
G limit ≈ -5/13 G
Gear Speed Limit (IAS) 426 km/h
Suspended armament
Max weight 3,000 kg
Wing loading left / right
Maximum 1,000 kg
Max. difference 1,000 kg

NameWeightSlot
76.4 kg
117.3 kg
Start JATO rocket booster100 kg
2 × 222.9 kg
Additional fuel tank for SEPR 8441 kg
2 × 800 kg
Drop tank (730 liters.)120 kg
SEPR 844 liquid-propellant rocket booster
Fuel tank for SEPR 844
211 kg
Conformal fuel tank1 kg
Start JATO rocket booster100 kg
Economy
Repair cost Basic → Reference
AB 3,089 → 4,155 SL
RB 10,079 → 13,556 SL
SB 9,280 → 12,482 SL
Crew training 200,000 SL
Experts 710,000 SL
Aces 2,800 GE
Research Aces 1,080,000 RP
Reward multiplier AB / RB / SB
120 / 340 / 600 % SL
232 % RP
Total cost of modifications 229,000 RP
356,000 SL
Talisman cost 2,800 GE

Research order:

Flight performance
Survivability
Weaponry
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