Спойлер
2.40.0.58 → 2.40.0.60 (2024-11-13)
Aircraft FM changes:
-
A-5C, Q-5A:
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
- will mean higher zero-lift drag coefficient peak at M1.03, resulting in lower top speed and more overall supersonic drag ( comparison picture, orange is new, blue is old )
- fuselage zero-lift drag coefficient increased from 0.005 to 0.0055
- will mean slightly lower top speed and slightly more overall drag
- afterburning thrust adjustments at 17000 m, 1000-1600 km/h TAS
- comparison picture, orange is new, blue is old. Overall reduction in thrust by ~300 kgf at 1200 km/h, ~200 kgf at 1400 km/h
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
-
Q-5:
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
- will mean higher zero-lift drag coefficient peak at M1.03, resulting in lower top speed and more overall supersonic drag ( comparison picture, orange is new, blue is old )
- fuselage zero-lift drag coefficient increased from 0.005 to 0.0055
- will mean slightly lower top speed and slightly more overall drag
- afterburning thrust adjustments at 17000 m, 1000-1600 km/h TAS
- comparison picture, orange is new, blue is old. Overall reduction in thrust by ~200 kgf at 1200 km/h, ~100 kgf at 1400 km/h
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
-
Q-5L:
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
- will mean higher zero-lift drag coefficient peak at M1.03, resulting in lower top speed and more overall supersonic drag ( comparison picture, orange is new, blue is old )
- fuselage zero-lift drag coefficient increased from 0.0051 to 0.0056
- will mean slightly lower top speed and slightly more overall drag
- afterburning thrust adjustments at 17000 m, 1000-1600 km/h TAS
- comparison picture, orange is new, blue is old. Overall reduction in thrust by ~300 kgf at 1200 km/h, ~200 kgf at 1400 km/h
- fuselage zero-lift drag coefficient Mach curve Mach multiplier max increased from 2.8 to 3.4
Aircraft DM changes:
- F-4J, F-4S: area where the HMD blocks the HUD: 0.2 / 0.2 / 0.63 / 0.63 → 0.25 / -0.4 / 0.65 / 0.75
- Gripen C [GBR], JAS 39A, JAS 39C, JAS 39C EBS HU: pilot: SWE late → USA 1977-1991
- J-11, J-11A, MiG-21 Bison, MiG-29 (9-12A) [DEU], MiG-29 (9-13), MiG-29G, MiG-29SMT, Mirage 2000 5F, Mirage 2000-5 EI, Su-27, Su-27SM, Yak-141: area where the HMD blocks the HUD re-added
- SuperHind: RWR: SPO-15 → Vinten (copy-paste)
Aircraft weapon changes:
- A-11B (“AMX”): loadout(s) changed: 1x 2000 lbs GBU-24/B: it now blocks flaps from opening more than 50%
- F-15E, F-15I Ra’am: loadout icons of the 3x 500 lbs GBU-38(V)1/B options still showed 6x, fixed
Sensor changes:
- ANTILOPE 5 (Mirage 2000 D RMV): added HMD lock, HMD track patterns
- V004 (Su-34):
- MPRF, HPRF transceivers: antenna: angle of half sensitivity: 3.5 → 1.5
- GTM transceiver: antenna: elevation: angle of half sensitivity: 3.5 → 1.5
- auto narrow search pattern:
- period: 0.5 → 1.8465887
- bar height: 3 → 1.5
- bar count: 4 → 8
- auto medium search pattern:
- period: 2 → 3.6931775
- bar height: 3 → 1.5
- auto wide search pattern:
- period: 3 → 6.4630604
- width: 45 → 30
- bar height: 3 → 1.5
- bar count: 8 → 16
- BVR lock search pattern: bar height: 3 → 1.5
- BVR lock TWS pattern:
- bar height: 3 → 1.5
- bar count: 2 → 4
- vertical lock pattern:
- bar height: 2.5 → 1.5
- bar count: 2 → 4
- centre elevation: 0° → 12.5°
- boresight lock pattern: width: 2 → 1.5
- HUD lock pattern: bar height: 2.5 → 1.5
Ground changes:
- HSTV(L), M1A2, Fiat 6616 (60 mm), Fiat 6616 (90 mm), KF41, CV90105 (XC-8), strv 122A, strv 122B (PLSS): added stock 800x600 driver NVD
- XM1069 (ADATS): coaxial MG: 12.7 mm M2 HB → 12.7 mm M3P
- Panther II, ZSU-23-4, ZSU-37-2, Vickers Mk. 3, ZSU-23-4 [ITA], ZSU-23-4 [ISR]: 800x600 driver and commander NVD are now available stock
- 2S25M: cannon vertical limits: -5° / 16° → -4° / 16°
- BMP-2D, BMP-2M, BMP-2MD: cannon recoil multiplier: 0.045 → 0.03
- T-80UE-1:
- unknown armour: 10 → 4 mm
- unknown armour: RHA → CHA
- ICV (P):
- added 10 mm RHA in unknown location
- added 4 mm RHA in unknown location
- added 4 mm RHA in unknown location
- removed 4 mm RHA turret rear roof hatches
- RCV (P):
- added 10 mm RHA in unknown location
- added 10 mm RHA in unknown location
- added 4 mm RHA in unknown location
- Magach 5: added stock 800x600 gunner NVD
- Sabra: cannon first stage size: 19 → 25
Aircraft weapon changes:
- 30 mm GIAT M781:
- rate of fire: 720 → 750 rpm
- SAPHEI:
- mass: 275 → 236 g
- speed: 810 → 820 m/s
- explosive mass: 14 → 50 g
- penetration: 28.92 → 26.41 mm
Ground weapon changes:
- 130 mm PL59A: DJF1 Smoke: mass: 33.47 → 33.77 kg
Features:
- allow radar mode options: no longer locked to devs
- hit analysis: no longer available on consoles
Statcard and X-Ray changes:
- Ki 67 Kō, Ki 67 Otsu: fuel tanks No. 2, 3, 4 and 5 are now marked as self-sealing with neutral gas pressurisation system in X-Ray
Economy changes:
- Panther II:
- minimum repair cost: 904 / 897 / 899 → 976 / 967 / 970 SL/minute
- full stock repair cost: 3637 / 4143 / 5400 → 3924 / 4470 / 5826 SL
- number of modifications needed to unlock Tier 4: 3 → 2
- modification changes:
- removed NVD modification
- Horizontal Drive:
- repair cost coefficient: 0.015 → 0.014
- GE cost: 260 → 250
- Tracks:
- repair cost coefficient: 0.015 → 0.014
- GE cost: 260 → 250
- Improved Parts: GE cost: 260 → 250
- Gr. 39 HL HEAT (modification): GE cost: 175 → 165
- Improved FPE: GE cost: 175 → 165
- Brake System:
- repair cost coefficient: 0.019 → 0.018
- GE cost: 175 → 165
- Suspension:
- repair cost coefficient: 0.012 → 0.011
- GE cost: 175 → 165
- Adjustment of Fire:
- repair cost coefficient: 0.024 → 0.022
- GE cost: 175 → 165
- Filters:
- repair cost coefficient: 0.037 → 0.034
- RP cost: 4000 → 5000
- SL cost: 6500 → 8100
- GE cost: 195 → 230
- Elevation Mechanism:
- repair cost coefficient: 0.034 → 0.032
- RP cost: 4000 → 5000
- SL cost: 6500 → 8100
- GE cost: 195 → 230