MI-C.A.D.O.

MI-C.A.D.O. 3view

Japanese/English

MI-C.A.D.O./MI-C.A.D.O. II

The MI-C.A.D.O. stands for the Multi purpose Intercepter-Computer Assisted Direct Operation.
At first the MI-C.A.D.O. is developed as a special tactical strike fighter for NAA by APEN. But APEN use it for own main fighter.
The MI-C.A.D.O. has the composite structure of conventional material and new material made in the orbit.
And it has a new engine developed by Mutsubishi Heavy Industries.
For that reason it has a high maneuverability and a lot of payloads.
sub-types are shown as bellow.

F-04B:first model
F-04BII:enhanced the numbers of AAMs from 4 to 6
F-04BIII:enhanced invulnerability
F-04C:guidance of 2 missiles simultaneously and enhanced AAM range by 50%
F-04C(mod):enhanced the numbers of AAMs from 6 to 10

MI-C.A.D.O. II 3D models and specifications.
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A prototype of F-04C from the cockpit of F-04B II
(The mountain in the background is Mt. Fuji)

MI-C.A.D.O. III

The F-04D MI-C.A.D.O. III is developed for war against the isomer.
It has been modefied from F-04C, a engine replacement and addition of a gravity control unit.
The result of this modification, the weight is pretty increased. But it can cruise up to Mach 3 and has a super maneuverability enough to need a genetic recombination pilot.

Comparison of the characteristics
F-04C MI-C.A.D.O. IIF-04D MI-C.A.D.O. III
Length16.4m16.4m
Wingspan9.86m9.86m
Height5.64m5.64m
Wing area37.6m237.6m2
Operational weight6980kg7540kg
Maximum takeoff weight12300kg22500kg
EngineM-21-ML-004DM-21-ML-005D
Thrust14850kg x139330kg x1
Gravity control unit-GMC-02
Maximum power-0.8G
SpeedM2.4M3.75
Super cruise-M3.18
Stall speed-M0.05
Ceiling18000m18000m
Range3800km3800kg
Combat radius900km900kg
Fuel3100kg4500kg
Take off450m45m
Landing730m18m
internal weapon30mm rail gun x230mm rail gun x2
Hard point55
Crew11

Fligt envelope

Level flight envelopes of F-04C MI-C.A.D.O.II and F-04D MI-C.A.D.O.III are shown as follow.

Level Flight Envelope


Copyright(c) FLIGHT SIM HERITAGE 2001. All Rights Reserved.

Some material copyright SystemSoft (c) 1990, 2001.
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