JX-2, a lightweight single engine version based on the new design of JX-1.The high thrust engine of the same model JX-1 is used, which has greater internal oil and acceleration performance.
JX-2 supersonic single engine fighter, with an empty weight of 7.9t, a maximum internal fuel of 8t, a maximum hang of 4t, and a recommended takeoff mass of less than 16t. This mode has a takeoff mass of 15.5t, carrying 5.5t fuel and 2t ammunition.
Activation Groups
1.Engine
2.Cookpit Canopy
3.Landing Gear
4.DC-1(left)
5.DC-1(right)
6.DC-2(outside)
7.DC-2(Medial side)
8.Built-in bomb chamber
9.Discard ZC-1
10.ZC-1
Two DC-1 air-to-air missiles and two DC-2 air-to-air missiles are mounted outside the wing, and two DC-2 air-to-air missiles are carried in the side missile compartment. (Technical problems can only be controlled manually or inertial flight) At the same time, a brand new glide bomb ZC-1 is attached to the belly of the aircraft, which needs to be controlled manually. Click the "10" activation group to start the engine and fold the wing. The fuel volume controls the expansion angle. Try not to fully expand the wing at supersonic speed to avoid wing explosion.
GENERAL INFO
- Predecessor: JX-1
- Successors 3 craft(s)
- Created On: Android
- Game Version: 0.9.914.0
- Price: $14,630k
- Number of Parts: 256
- Dimensions: 6 m x 11 m x 16 m
PERFORMANCE
- Total Delta V: 86m/s
- Total Thrust: 730kN
- Engines: 9
- Wet Mass: 6,943kg
- Dry Mass: 8,574kg
STAGES
| Stage | Engines | Delta V | Thrust | Burn | Mass |
|---|---|---|---|---|---|
| 1 | 1 | 0m/s | 0N | 0s | 15,517kg |
| 2 | 7 | 86m/s | 730kN | 6s | 15,517kg |
4 Comments
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1,989 Remember9182.1 years ago
Solution to wing explosion of ZC-1 glider missile.
"TINKER PANEL"→Edit Hidden Properties→<Wing>→Wing Strength override -1 -
1,989 Remember9182.2 years ago
Gliding missile "ZC-1" should not fully extend its wings and maneuver with heavy overload at supersonic speed to avoid explosion. Sorry, the first generation glider missile is defective.
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Correction of design error: change the vertical tail control surface to YAW.