Comments (6)
NexitySecond
commented on June 3, 2024
ok
from roblox-4.
Itzbenz
commented on June 3, 2024
@thisgary
from roblox-4.
garylkz
commented on June 3, 2024
You use python script so it's nanomybusiness
from roblox-4.
NexitySecond
commented on June 3, 2024
help there is a terrorist among us
from roblox-4.
garylkz
commented on June 3, 2024
there's an issue
spills nonsense
close issue
from roblox-4.
NexitySecond
commented on June 3, 2024
-- Simplified Aerodynamic Model by Helmo
-- mounting 3d model paths and texture paths
--mount_vfs_model_path (current_mod_path.."/Shapes")
--mount_vfs_liveries_path (current_mod_path.."/Liveries") -- mounted in entry.lua
--mount_vfs_texture_path (current_mod_path.."/Textures") -- mounted in entry.lua
local KG_TO_POUNDS = 2.20462
local POUNDS_TO_KG = 1/KG_TO_POUNDS
local FEET_TO_M = 0.3048
--------------------------------------------Colt MK12 Gun----------------------------------------------------------------------------
local function coltMK12(tbl)
tbl.category = CAT_GUN_MOUNT
tbl.name = "coltMK12"
tbl.supply =
{
shells = {"20x110mm HE-I", "20x110mm AP-I", "20x110mm AP-T"},
mixes = {{1,2,1,2,1,3}}, -- 50% HE-i, 25% AP-I, 25% AP-T
count = 100,
}
if tbl.mixes then
tbl.supply.mixes = tbl.mixes
tbl.mixes = nil
end
tbl.gun =
{
max_burst_length = 100000,
rates = {1000},
recoil_coeff = 0.7*1.3,
barrels_count = 1,
}
if tbl.rates then
tbl.gun.rates = tbl.rates
tbl.rates = nil
end
tbl.ejector_pos = tbl.ejector_pos or {0, 0, 0}
tbl.ejector_pos_connector = tbl.ejector_pos_connector or "Gun_point"
tbl.ejector_dir = {-1, -6, 0} -- left/right; back/front;?/?
tbl.supply_position = tbl.supply_position or {0, 0.3, -0.3}
tbl.aft_gun_mount = false
tbl.effective_fire_distance = 1500
tbl.drop_cartridge = 204
tbl.muzzle_pos = tbl.muzzle_pos or {0,0,0} -- all position from connector
tbl.muzzle_pos_connector = tbl.muzzle_pos_connector or "Gun_point" -- all position from connector
tbl.azimuth_initial = tbl.azimuth_initial or 0
tbl.elevation_initial = tbl.elevation_initial or 0
if tbl.effects == nil then
tbl.effects = {{ name = "FireEffect" , arg = tbl.effect_arg_number or 436 },
{ name = "HeatEffectExt" , shot_heat = 7.823, barrel_k = 0.462 * 2.7, body_k = 0.462 * 14.3 },
{ name = "SmokeEffect"}}
end
return declare_weapon(tbl)
end
local function get_outboard_weapons( side )
local rocketConnector = ""
local shrikeConnector = ""
if side == "L" then
rocketConnector = "Pylon1RKT"
shrikeConnector = "Pylon1b"
elseif side == "R" then
rocketConnector = "Pylon5RKT"
shrikeConnector = "Pylon5b"
end
local tbl = {
--ROCKETS--
--{ CLSID = "{FD90A1DC-9147-49FA-BF56-CB83EF0BD32B}" }, -- LAU-61, M151 HE
--{ CLSID = "{174C6E6D-0C3D-42ff-BCB3-0853CB371F5C}" }, -- LAU 68, MK5 HE
{ CLSID = "{F3EFE0AB-E91A-42D8-9CA2-B63C91ED570A}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-10 Zuni
{ CLSID = "{LAU3_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-3 FFAR WP156
{ CLSID = "{LAU3_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-3 FFAR Mk1 HE
{ CLSID = "{LAU3_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-3 FFAR Mk5 HEAT
{ CLSID = "{LAU68_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR WP156
{ CLSID = "{LAU68_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU68_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk5 HEAT
--MISSILES--
{ CLSID = "{AGM_45A}", connector = shrikeConnector, arg_value = 0.1 }, -- AGM-45 SHRIKE
{ CLSID = "{AGM12_B}" }, -- AGM-12B
--BOMBS--
{ CLSID = "{ADD3FAE1-EBF6-4EF9-8EFC-B36B5DDF1E6B}" }, -- Mk-20 Rockeye cluster bomb
{ CLSID = "{90321C8E-7ED1-47D4-A160-E074D5ABD902}" }, -- MK-81
{ CLSID = "{MK-81SE}" }, -- Mk-81 Snakeye
{ CLSID = "{BCE4E030-38E9-423E-98ED-24BE3DA87C32}" }, -- MK-82
{ CLSID = "{Mk82SNAKEYE}" }, -- MK-82 Snakeye
{ CLSID = "{mk77mod1}" }, -- Mk-77mod1 500 lb petroleum oil bomb
{ CLSID = "{AN-M30A1}" }, -- AN-M30A1 100 lb GP HE (57 lb TNT)
{ CLSID = "{AN-M57A1}" }, -- AN-M57A1 250 lb GP HE (129 lb TNT)
{ CLSID = "{AN-M64}" }, -- AN-M64 500 lb GP HE (274 lb Comp B)
{ CLSID = "{AN-M81}" }, -- AN-M81 260 lb Fragmentation (34.1 lb Comp B)
{ CLSID = "{AN-M88}" }, -- AN-M88 216 lb Fragmentation (47 lb Comp B)
--SPECIAL--
{ CLSID = "{647C5F26-BDD1-41e6-A371-8DE1E4CC0E94}"}, -- temporarily add M257 parachute flares until we can add: Mk-5 mod 7, Mk-6 mod 5, Mk-24 mod 2A, SUU-40/44
-- SMOKE PODS --
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E741}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Red
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E742}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Green
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E743}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Blue
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E744}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod White
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E745}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Yellow
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E746}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Orange
-- CLEAN --
{ CLSID = "<CLEAN>", arg_value = 1 },
}
return tbl
end
local function get_inboard_weapons( side )
local rocketConnector = ""
local shrikeConnector = ""
if side == "L" then
rocketConnector = "Pylon2RKT"
shrikeConnector = "Pylon2b"
elseif side == "R" then
rocketConnector = "Pylon4RKT"
shrikeConnector = "Pylon4b"
end
local tbl = {
--FUEL TANKS--
{ CLSID = "{DFT-300gal_LR}" },
-- { CLSID = "{DFT-300gal_LR}",attach_point_position = { -0.10, -0.008, 0.0}}, --another (proper?) posibility to fix 300 gal tank position/angle ?
{ CLSID = "{DFT-150gal}" },
--AIR AIR--
{ CLSID = "{GAR-8}", connector = rocketConnector, arg_value = 0.2 }, -- AIM-9B, aligned to -3deg armament datum
{ CLSID = "{AIM-9P-ON-ADAPTER}", connector = rocketConnector, arg_value = 0.2 }, -- AIM-9P
{ CLSID = "{AIM-9P5-ON-ADAPTER}", connector = rocketConnector, arg_value = 0.2 }, -- AIM-9P5
--ROCKETS--
{ CLSID = "{F3EFE0AB-E91A-42D8-9CA2-B63C91ED570A}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-10 Zuni
{ CLSID = "{LAU-10 ZUNI_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-10 Zuni
{ CLSID = "{LAU3_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU3_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU3_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU-3 FFAR WP156_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR WP156
{ CLSID = "{LAU-3 FFAR Mk1 HE_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR Mk1 HE
{ CLSID = "{LAU-3 FFAR Mk5 HEAT_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR Mk5 HEAT
{ CLSID = "{LAU68_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR WP156
{ CLSID = "{LAU68_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU68_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk5 HEAT
{ CLSID = "{LAU-68 FFAR WP156_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR WP156
{ CLSID = "{LAU-68 FFAR Mk1 HE_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU-68 FFAR Mk5 HEAT_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR Mk5 HEAT
--MISSILES--
{ CLSID = "{AGM_45A}", connector = shrikeConnector, arg_value = 0.1 }, -- AGM-45 SHRIKE
{ CLSID = "{AGM12_C}" }, -- AGM-12C
{ CLSID = "{AGM12_B}" }, -- AGM-12B
--BOMBS--
{ CLSID = "{C40A1E3A-DD05-40D9-85A4-217729E37FAE}" }, -- AGM-62 WALLEYE
{ CLSID = "{ADD3FAE1-EBF6-4EF9-8EFC-B36B5DDF1E6B}" }, -- Mk-20 Rockeye cluster bomb
{ CLSID = "{90321C8E-7ED1-47D4-A160-E074D5ABD902}" }, -- MK-81
{ CLSID = "{MK-81SE}" }, -- Mk-81 Snakeye
{ CLSID = "{BCE4E030-38E9-423E-98ED-24BE3DA87C32}" }, -- MK-82
{ CLSID = "{Mk82SNAKEYE}" }, -- MK-82 Snakeye
{ CLSID = "{7A44FF09-527C-4B7E-B42B-3F111CFE50FB}" }, -- MK-83
{ CLSID = "{AB8B8299-F1CC-4359-89B5-2172E0CF4A5A}" }, -- MK-84
{ CLSID = "{00F5DAC4-0466-4122-998F-B1A298E34113}" }, -- M-117
{ CLSID = "{mk77mod0}" }, -- Mk-77mod0 750 lb petroleum oil bomb
{ CLSID = "{mk77mod1}" }, -- Mk-77mod1 500 lb petroleum oil bomb
{ CLSID = "{AN-M30A1}" }, -- AN-M30A1 100 lb GP HE (57 lb TNT)
{ CLSID = "{AN-M57A1}" }, -- AN-M57A1 250 lb GP HE (129 lb TNT)
{ CLSID = "{AN-M64}" }, -- AN-M64 500 lb GP HE (274 lb Comp B)
{ CLSID = "{AN-M65A1}" }, -- AN-M65A1 1000 lb GP HE (595 lb Comp B)
{ CLSID = "{AN-M81}" }, -- AN-M81 260 lb Fragmentation (34.1 lb Comp B)
{ CLSID = "{AN-M88}" }, -- AN-M88 216 lb Fragmentation (47 lb Comp B)
--CLUSTER MUNITIONS--
{ CLSID = "{CBU-1/A}" }, -- CBU-1/A Cluster Dispenser (509x BLU-4/B anti-personnel cluster bomblets)
{ CLSID = "{CBU-2/A}" }, -- CBU-2/A Cluster Dispenser (360x BLU-3/B cluster bomblets)
{ CLSID = "{CBU-2B/A}" }, -- CBU-2B/A Cluster Dispenser (409x BLU-3/B cluster bomblets)
{ CLSID = "{CBU-1/A_TER_2_"..side.."}" }, -- CBU-1/A Cluster Dispenser x2 (509x BLU-4/B anti-personnel cluster bomblets)
{ CLSID = "{CBU-2/A_TER_2_"..side.."}" }, -- CBU-2/A Cluster Dispenser x2 (360x BLU-3/B cluster bomblets)
{ CLSID = "{CBU-2B/A_TER_2_"..side.."}" }, -- CBU-2B/A Cluster Dispenser x2 (409x BLU-3/B cluster bomblets)
-- BOMB RACKS --
{ CLSID = "{Mk-20_TER_2_"..side.."}" }, -- Mk-20 Rockeye cluster bomb x2
{ CLSID = "{Mk-81_MER_5_"..side.."}" }, -- MER Mk-81 x5
{ CLSID = "{Mk-81SE_MER_5_"..side.."}" }, -- MER Mk-81 Snakeye x5
{ CLSID = "{Mk-82_TER_2_"..side.."}" }, -- TER Mk-82 x2
{ CLSID = "{Mk-82 Snakeye_TER_2_"..side.."}" }, -- TER Mk-82 Snakeye x2
{ CLSID = "{AN-M57A1_MER_5_"..side.."}" }, -- AN-M57A1 x5 250 lb GP HE (129 lb TNT)
{ CLSID = "{AN-M81_MER_5_"..side.."}" }, -- AN-M81 x5 260 lb Fragmentation (34.1 lb Comp B)
{ CLSID = "{AN-M88_MER_5_"..side.."}" }, -- AN-M88 x5 216 lb Fragmentation (47 lb Comp B)
-- GUN PODS --
{CLSID = "{Mk4 HIPEG}", connector = rocketConnector, arg_value = 0.2 }, -- Mk 4 Mod 0 HIPEG gun pod
-- SMOKE PODS --
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E741}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Red
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E742}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Green
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E743}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Blue
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E744}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod White
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E745}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Yellow
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E746}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Orange
-- CLEAN --
{ CLSID = "<CLEAN>", arg_value = 1 },
}
return tbl
end
local function get_centerline_weapons( side )
local rocketConnector = "Pylon3RKT"
local tbl = {
--FUEL TANKS--
{ CLSID = "{DFT-400gal}" },
{ CLSID = "{DFT-300gal}" },
{ CLSID = "{DFT-150gal}" },
{ CLSID = "{D-704_BUDDY_POD}" },
--ROCKETS--
{ CLSID = "{3*LAU-61}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{9BC82B3D-FE70-4910-B2B7-3E54EFE73262}", connector = rocketConnector, arg_value = 0.2 }, --3*LAU 68, MK5 HE
{ CLSID = "{F3EFE0AB-E91A-42D8-9CA2-B63C91ED570A}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-10 Zuni
{ CLSID = "{LAU-10 ZUNI_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-10 Zuni
{ CLSID = "{LAU-10 ZUNI_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-10 Zuni
{ CLSID = "{LAU3_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU3_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU3_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 },
{ CLSID = "{LAU-3 FFAR WP156_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR WP156
{ CLSID = "{LAU-3 FFAR Mk1 HE_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR Mk1 HE
{ CLSID = "{LAU-3 FFAR Mk5 HEAT_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-3 FFAR Mk5 HEAT
{ CLSID = "{LAU-3 FFAR WP156_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-3 FFAR WP156
{ CLSID = "{LAU-3 FFAR Mk1 HE_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-3 FFAR Mk1 HE
{ CLSID = "{LAU-3 FFAR Mk5 HEAT_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-3 FFAR Mk5 HEAT
{ CLSID = "{LAU68_FFAR_WP156}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR WP156
{ CLSID = "{LAU68_FFAR_MK1HE}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU68_FFAR_MK5HEAT}", connector = rocketConnector, arg_value = 0.2 }, -- LAU-68 FFAR Mk5 HEAT
{ CLSID = "{LAU-68 FFAR WP156_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR WP156
{ CLSID = "{LAU-68 FFAR Mk1 HE_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU-68 FFAR Mk5 HEAT_TER_2_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Dual LAU-68 FFAR Mk5 HEAT
{ CLSID = "{LAU-68 FFAR WP156_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-68 FFAR WP156
{ CLSID = "{LAU-68 FFAR Mk1 HE_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-68 FFAR Mk1 HE
{ CLSID = "{LAU-68 FFAR Mk5 HEAT_TER_3_"..side.."}", connector = rocketConnector, arg_value = 0.2 }, -- Triple LAU-68 FFAR Mk5 HEAT
--MISSILES--
{ CLSID = "{AGM12_B}" }, -- AGM-12B
--BOMBS--
{ CLSID = "{C40A1E3A-DD05-40D9-85A4-217729E37FAE}" }, -- AGM-62 WALLEYE
{ CLSID = "{ADD3FAE1-EBF6-4EF9-8EFC-B36B5DDF1E6B}" }, -- Mk-20 Rockeye cluster bomb
{ CLSID = "{90321C8E-7ED1-47D4-A160-E074D5ABD902}" }, -- MK-81
{ CLSID = "{MK-81SE}" }, -- Mk-81 Snakeye
{ CLSID = "{BCE4E030-38E9-423E-98ED-24BE3DA87C32}" }, -- MK-82
{ CLSID = "{Mk82SNAKEYE}" }, -- MK-82 Snakeye
{ CLSID = "{7A44FF09-527C-4B7E-B42B-3F111CFE50FB}" }, -- MK-83
{ CLSID = "{AB8B8299-F1CC-4359-89B5-2172E0CF4A5A}" }, -- MK-84
{ CLSID = "{00F5DAC4-0466-4122-998F-B1A298E34113}" }, -- M117
{ CLSID = "{mk77mod0}" }, -- Mk-77mod0 750 lb petroleum oil bomb
{ CLSID = "{mk77mod1}" }, -- Mk-77mod1 500 lb petroleum oil bomb
{ CLSID = "{AN-M30A1}" }, -- AN-M30A1 100 lb GP HE (57 lbs TNT)
{ CLSID = "{AN-M57A1}" }, -- AN-M57A1 250 lb GP HE (129 lbs TNT)
{ CLSID = "{AN-M64}" }, -- AN-M64 500 lb GP HE (274 lbs Comp B)
{ CLSID = "{AN-M65A1}" }, -- AN-M65A1 1000 lb GP HE (595 lb Comp B)
{ CLSID = "{AN-M66A2}" }, -- AN-M66A2 2000 lb GP HE (1142 lb Comp B)
{ CLSID = "{AN-M81}" }, -- AN-M81 260 lb Fragmentation (34.1 lb Comp B)
{ CLSID = "{AN-M88}" }, -- AN-M88 216 lb Fragmentation (47 lb Comp B)
--BOMB RACKS--
{ CLSID = "{Mk-20_TER_3_"..side.."}" }, -- Mk-20 Rockeye cluster bomb x3
{ CLSID = "{Mk-20_TER_2_"..side.."}" }, -- Mk-20 Rockeye cluster bomb x2
{ CLSID = "{Mk-81_MER_6_"..side.."}" },
{ CLSID = "{Mk-81SE_MER_6_"..side.."}" }, -- MER Mk-81 Snakeye x6
{ CLSID = "{Mk-82_MER_6_"..side.."}" },
{ CLSID = "{Mk-82_MER_4_"..side.."}" },
{ CLSID = "{Mk-82_TER_3_"..side.."}" },
{ CLSID = "{Mk-82 Snakeye_MER_6_"..side.."}" },
{ CLSID = "{Mk-82 Snakeye_MER_4_"..side.."}" },
{ CLSID = "{Mk-82 Snakeye_TER_3_"..side.."}" },
{ CLSID = "{Mk-83_TER_3_"..side.."}" },
{ CLSID = "{Mk-83_TER_2_"..side.."}" },
{ CLSID = "{Mk-77 mod 1_TER_2_"..side.."}" }, -- Mk-77 mod 1 (500 lb) x2 petroleum oil bomb
{ CLSID = "{AN-M57A1_MER_6_"..side.."}" }, -- AN-M57A1 x6 250 lb GP HE (129 lb TNT)
{ CLSID = "{AN-M57A1_MER_4_"..side.."}" }, -- AN-M57A1 x4 250 lb GP HE (129 lb TNT)
{ CLSID = "{AN-M81_MER_6_"..side.."}" }, -- AN-M81 x6 260 lb Fragmentation (34.1 lb Comp B)
{ CLSID = "{AN-M88_MER_6_"..side.."}" }, -- AN-M88 x6 216 lb Fragmentation (47 lb Comp B)
-- GUN PODS --
{CLSID = "{Mk4 HIPEG}", connector = rocketConnector, arg_value = 0.2 }, -- Mk 4 Mod 0 HIPEG gun pod
-- SMOKE PODS --
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E741}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Red
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E742}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Green
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E743}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Blue
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E744}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod White
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E745}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Yellow
{CLSID = "{A4BCC903-06C8-47bb-9937-A30FEDB4E746}", connector = rocketConnector, arg_value = 0.2 }, -- Smoke Pod Orange
-- CLEAN --
{ CLSID = "<CLEAN>", arg_value = 1 },
}
return tbl
end
A_4E_C = {
Name = 'A-4E-C',
DisplayName = _('A-4E-C'),
ViewSettings = ViewSettings,
-- enable A-4 for all countries. It is CHEAP and easy to maintain
Countries = {"Abkhazia","Australia","Austria","Belarus","Belgium","Brazil","Bulgaria","Canada","China","Croatia",
"Czech Republic","Denmark","Egypt","Finland","France","Georgia","Germany","Greece","Hungary",
"India","Insurgents","Iran","Iraq","Israel","Italy","Japan","Kazakhstan","The Netherlands","North Korea",
"Norway","Pakistan","Poland","Romania","Russia","Saudi Arabia","Serbia","Slovakia","South Korea",
"South Ossetia","Spain","Sweden","Switzerland","Syria","Turkey","UK","Ukraine","USA","USAF Aggressors"},
HumanCockpit = false,
HumanCockpitPath = current_mod_path..'/Cockpit/',
Picture = "A-4E-C.png",
Rate = 40, -- RewardPoint in Multiplayer
Shape = "A-4E",
shape_table_data =
{
{
file = 'A-4E';
life = 16; -- lifebar
vis = 3; -- visibility gain.
desrt = 'Fighter-2-crush'; -- Name of destroyed object file name Alphajet-destr. This is a placeholder.
fire = {300, 3}; -- Fire on the ground after destoyed: 300sec 2m
username = 'A-4E-C';
index = WSTYPE_PLACEHOLDER;
classname = "lLandPlane";
positioning = "BYNORMAL";
},
-- no need for this as we are using a built in destroyed model
-- {
-- name = "Alphajet-destr";
-- file = "Alphajet-destr";
-- fire = {240, 2}; -- 240 2
-- },
},
-------------------------
-- add model draw args for network transmitting to this draw_args table (32 limit)
net_animation ={
0, -- front gear
3, -- right gear
5, -- left gear
9, -- right flap
10, -- left flap
11, -- right aileron
12, -- left aileron
15, -- right elevator
16, -- left elevator
17, -- rudder
2, -- nose wheel steering
21, -- SFM air brake
13, -- right slat
14, -- left slat
25, -- tail hook
38, -- canopy
120, -- right spoiler
123, -- left spoiler
190, -- left (red) navigation wing-tip light
191, -- right (green) navigation wing-tip light
192, -- tail (white) light
198, -- anticollision (flashing red) top light
199, -- anticollision (flashing red) bottom light
208, -- taxi light (white) right main gear door
402, --huffer
500, -- model air brake
501, -- RAT
499, -- wheel chocks
},
-------------------------
mapclasskey = "P0091000024",
attribute = {wsType_Air, wsType_Airplane, wsType_Fighter, WSTYPE_PLACEHOLDER, "Multirole fighters", "Refuelable" },
Categories = {"{78EFB7A2-FD52-4b57-A6A6-3BF0E1D6555F}", "Interceptor",},
-------------------------
-- Operating Weight includes: centerline rack, crew, engine oil, trapped fuel and oil, liquid oxygen, avionics pod, ECM, and misc equipment
-- A-4E: 10,802 lbs operating weight
-- + 314 lbs for 2x 20mm cannon (no ammo)
-- + 140 lbs for 2x AERO 20A rack pylons on stations 2/4
-- + 128 lbs for 2x AERO 20A rack pylons on stations 1/5
-- +*398 lbs for 2x empty AERO-1D empty 300G fuel tanks
-- + 97 lbs for armor plating
-- + 32 lbs for wing spoilers
-- + 76 lbs for J52-P-8A engine (versus J52-P-6A)
-- ------
-- TOTAL: 11,589 lbs with no ammo, no gas, and empty pylons
M_empty = 11589*POUNDS_TO_KG, -- see above calculation
M_nominal = 17180*POUNDS_TO_KG, -- combat weight per NATOPS
M_max = 24500*POUNDS_TO_KG, -- (Maximum Take Off Weight)
M_fuel_max = 5440*POUNDS_TO_KG, -- (Internal Fuel Only) : 800G * ~6.8 lbs/gal for JP-5
H_max = 43900*FEET_TO_M, -- m (Maximum Operational Ceiling) : Combat ceiling @ 14,500 lbs w/ 500 fpm climb max
-------------------------
length = 12.22, -- full lenght in m
height = 4.57, -- height in m
wing_area = 24.16, -- wing area in m2 **
wing_span = 8.38 , -- wing span in m
wing_tip_pos = {-2.5, -0.38, 4.2}, -- wingtip coords for visual effects
wing_type = 0, -- FIXED_WING = 0 /VARIABLE_GEOMETRY = 1 /FOLDED_WING = 2 /ARIABLE_GEOMETRY_FOLDED = 3
flaps_maneuver = 0.5, -- Max flaps in take-off and maneuver (0.5 = 1st stage; 1.0 = 2nd stage) (for AI)
has_speedbrake = true,
RCS = 3.4, -- Radar Cross Section m2. Proportionally scaled RCS of F-16's 4.0.
IR_emission_coeff = 0.275, -- Normal engine -- IR_emission_coeff = 1 is Su-27 without afterburner. It is reference. 33,820 lbf dry for Su-27. 9300 lbf dry A-4 = 0.275
IR_emission_coeff_ab = 0.275, -- With afterburner
stores_number = 5, -- Amount of pylons.
CAS_min = 25.7, -- minimal indicated airspeed m/s? (50 knots per NATOPS)
V_opt = 200, -- Cruise speed (for AI)
V_take_off = 82.3, -- Take off speed in m/s (for AI - 150kts)
V_land = 64.3, -- Land speed in m/s (for AI) (110 kn)
V_max_sea_level = 300.83, -- Max speed at sea level in m/s (for AI)
V_max_h = 300.8, -- Max speed at max altitude in m/s (for AI)
Vy_max = 102.9, -- Max climb speed in m/s (for AI - 200 kts)
Mach_max = 0.88, -- Max speed in Mach (for AI)
Ny_min = -3.0, -- Min G (for AI)
Ny_max = 8.0, -- Max G (for AI)
Ny_max_e = 8.0, -- Max G (for AI)
--AOA_take_off = 0.27, -- AoA in take off radians (for AI) 16 degrees
bank_angle_max = 60, -- Max bank angle (for AI)
range = 3200, -- Max range in km (for AI)
thrust_sum_max = 9300*POUNDS_TO_KG, -- thrust in kg (J52 P8A: 9300 lb) **
has_afteburner = true,
has_differential_stabilizer = false,
thrust_sum_ab = 9300*POUNDS_TO_KG, -- thrust in kg (kN) **
average_fuel_consumption = 0.86, -- 0.86 TSFC
is_tanker = false,
tanker_type = 2, -- Tanker type if the plane is tanker
air_refuel_receptacle_pos = {6.966, -0.366, 0.486},
-----------------------------------------------------------------------
----------------- SUSPENSION CODE BEGINS
-----------------------------------------------------------------------
nose_gear_pos = {2.72, -2.38, 0}, --{2.72, -2.37, 0}, -- 2.72, -2.28, 0
main_gear_pos = {-0.79, -2.46, 1.18}, --{-0.79, -2.42, 1.18}, -- 0.79, -2.35, 1.18
tand_gear_max = 0.554, -- // tangent on maximum yaw angle of front wheel
nose_gear_amortizer_direct_stroke = 0.05, --1.878 - 1.878, -- down from nose_gear_pos !!!
nose_gear_amortizer_reversal_stroke = -0.32, --1.348 - 1.878, -- up
main_gear_amortizer_direct_stroke = 0.0, --1.592 - 1.592, -- down from main_gear_pos !!!
main_gear_amortizer_reversal_stroke = -0.43, --1.192 - 1.592, -- up
nose_gear_amortizer_normal_weight_stroke = -0.20, -- 0.144
main_gear_amortizer_normal_weight_stroke = -0.51, --
nose_gear_wheel_diameter = 0.441, --0.441, --*
main_gear_wheel_diameter = 0.609, --0.609, --*
brakeshute_name = 0, -- Landing - brake chute visual shape after separation
-----------------------------------------------------------------------
----------------- SUSPENSION CODE ENDS
-----------------------------------------------------------------------
engines_count = 1,
engines_nozzles =
{
[1] =
{
pos = {-5.62, 0.163, 0}, -- nozzle coords
elevation = 0.0, -- AFB cone elevation
-- Diameter is 0 to hide AB for AI. AB is used for catapult simulation.
-- If AB is no longer used for catapult then diameter can be set for exhaust smoke.
diameter = 0.0, -- AFB cone diameter.
-- diameter = 0.675, -- AFB cone diameter
exhaust_length_ab = 0, -- lenght in m
exhaust_length_ab_K = 0.707, -- AB animation
smokiness_level = 0.15,
}, -- end of [1]
}, -- end of engines_nozzles
crew_size = 1,
crew_members =
{
[1] =
{
ejection_seat_name = 17,
drop_canopy_name = "A-4E_canopy", --23,
pos = {3.077, -0.03, 0}, --changes the position of the cockpit view {3.077, 0.574, 0}
canopy_pos = {3.077, 0.674, 0},
-- canopy_pos = {2.677,2.677,0},
--ejection_play_arg = 149,
--can_be_playable = true,
--ejection_through_canopy = true,
--ejection_added_speed = {-5,15,0},
--ejection_order = 2,
--role = "pilot",
--role_display_name = _("Pilot"),
g_suit = 5 -- I'm assuming there are different levels of suits which black you out at different G's. We should try and experiment with different ones.
}, -- end of [1]
}, -- end of crew_members
fires_pos =
{
[1] = {-0.232, 1.262, 0}, -- Fuselage
[2] = {-0.2, -0.5, 0.84}, -- wing (inner?) right, WING_R_IN
[3] = {-0.75, -0.5, -0.8}, -- wing (inner?) left, WING_L_IN
[4] = {-0.32, 0.265, 1.774}, -- Wing center Right? {-0.82, 0.265, 2.774},
[5] = {-0.32, 0.265, -1.774}, -- Wing center Left? {-0.82, 0.265, -2.774},
[6] = {-1.0, -0.5, 4.0}, -- Wing outer Right? {-0.82, 0.255, 4.274}, probably WING_R_OUT
[7] = {-1.0, -0.5, -4.0}, -- Wing outer Left? {-0.82, 0.255, -4.274}, probably WING_L_OUT
[8] = {-5.6, 0.185, 0}, -- High Altitude Contrails
[9] = {-5.5, 0.2, 0}, -- left engine
[10] = {-7.728, 0.039, 0.5}, -- Right Engine? {0.304, -0.748, 0.442},
[11] = {-7.728, 0.039, -0.5}, -- ?
}, -- end of fires_pos
-- --- Countermeasures---
-- SingleChargeTotal = 0,
-- CMDS_Incrementation = 1,
-- ChaffDefault = 0,
-- ChaffChargeSize = 1,
-- FlareDefault = 0,
-- FlareChargeSize = 1,
-- CMDS_Edit = false,
-- chaff_flare_dispenser = {
-- }, -- end of chaff_flare_dispenser
-- --- Countermeasures---
-- SingleChargeTotal = 128,
-- CMDS_Incrementation = 12,
-- ChaffDefault = 64,
-- ChaffChargeSize = 1,
-- FlareDefault = 64,
-- FlareChargeSize = 1,
-- CMDS_Edit = true,
passivCounterm = {
CMDS_Edit = true,
SingleChargeTotal = 60,
chaff = {default = 30, increment = 30, chargeSz = 1},
flare = {default = 30, increment = 30, chargeSz = 1},
},
chaff_flare_dispenser = {
-- althought the index here starts from 1. When calling drop_flares or drop_chaff, the index begins from 0
-- { dir = {Z, Y, X}, pos = {Z, Y, X}, } -- Z=back/fwd,Y=down/up(+),X=left/right
-- { dir = {-1, -0.1, -0.1}, pos = {-2.867, -0.6, -0.216}, }, -- Flares L
-- { dir = {-1, -0.1, 0.1}, pos = {-2.867, -0.6, 0.216}, }, -- Flares R
-- { dir = {-1, -1, 0}, pos = {-4.296, -0.429, 0}, }, -- Chaff aft 0
-- { dir = {-1, -1, 0}, pos = {-2.296, -0.429, 0}, }, -- Chaff fwd 1
[1] = { dir = {0, -1, 0}, pos = {-2.2, -0.8, 0.3}, }, -- Fwd Dispenser
-- [2] = { dir = {0, -1, 0}, pos = {-3.9, -0.8, -0.3}, }, -- Aft Dispenser
},
--sensors
detection_range_max = 250,
radar_can_see_ground = true,
CanopyGeometry = {
azimuth = {-160.0, 160.0}, -- pilot view horizontal (AI)
elevation = {-50.0, 90.0} -- pilot view vertical (AI)
},
Sensors = {
--RADAR = "AN/APG-53A",
IRST = "OLS-27",
OPTIC = "Shkval",--necessite un profil 25T.
RWR = "Abstract RWR"
},
Countermeasures = {
ECM = "AN/ALQ-165"
},
HumanRadio = {
frequency = 254.0, -- Maykop (Caucasus) or Nellis (NTTR)
editable = true,
minFrequency = 225.000,
maxFrequency = 399.900,
modulation = MODULATION_AM
},
panelRadio = {
[1] = {
name = _("AN/ARC-27A"),
range = {
{min = 225.0, max = 399.9}
},
channels = { -- matches L-39C except for channel 8, which was changed to a Georgian airport and #20 which is NTTR only (for now). This radio goes 1-20 not 0-19.
[1] = { name = _("Channel 1"), default = 264.0, modulation = _("AM"), connect = true}, -- mineralnye-vody (URMM) : 264.0
[2] = { name = _("Channel 2"), default = 265.0, modulation = _("AM")}, -- nalchik (URMN) : 265.0
[3] = { name = _("Channel 3"), default = 256.0, modulation = _("AM")}, -- sochi-adler (URSS) : 256.0
[4] = { name = _("Channel 4"), default = 254.0, modulation = _("AM")}, -- maykop-khanskaya (URKH), nellis (KLSV) : 254.0
[5] = { name = _("Channel 5"), default = 250.0, modulation = _("AM")}, -- anapa (URKA) : 250.0
[6] = { name = _("Channel 6"), default = 270.0, modulation = _("AM")}, -- beslan (URMO) : 270.0
[7] = { name = _("Channel 7"), default = 257.0, modulation = _("AM")}, -- krasnodar-pashkovsky (URKK) : 257.0
[8] = { name = _("Channel 8"), default = 258.0, modulation = _("AM")}, -- sukhumi-babushara (UGSS) : 255.0
[9] = { name = _("Channel 9"), default = 262.0, modulation = _("AM")}, -- kobuleti (UG5X) : 262.0
[10] = { name = _("Channel 10"), default = 259.0, modulation = _("AM")}, -- gudauta (UG23) : 259.0
[11] = { name = _("Channel 11"), default = 268.0, modulation = _("AM")}, -- tbilisi-soganlug (UG24) : 268.0
[12] = { name = _("Channel 12"), default = 269.0, modulation = _("AM")}, -- tbilisi-vaziani (UG27) : 269.0
[13] = { name = _("Channel 13"), default = 260.0, modulation = _("AM")}, -- batumi (UGSB) : 260.0
[14] = { name = _("Channel 14"), default = 263.0, modulation = _("AM")}, -- kutaisi-kopitnari (UGKO) : 263.0
[15] = { name = _("Channel 15"), default = 261.0, modulation = _("AM")}, -- senaki-kolkhi (UGKS) : 261.0
[16] = { name = _("Channel 16"), default = 267.0, modulation = _("AM")}, -- tbilisi-lochini (UGTB) : 267.0
[17] = { name = _("Channel 17"), default = 251.0, modulation = _("AM")}, -- krasnodar-center (URKI), creech (KINS) : 251.0
[18] = { name = _("Channel 18"), default = 253.0, modulation = _("AM")}, -- krymsk (URKW), mccarran (KLAS) : 253.0
[19] = { name = _("Channel 19"), default = 266.0, modulation = _("AM")}, -- mozdok (XRMF) : 266.0
[20] = { name = _("Channel 20"), default = 252.0, modulation = _("AM")}, -- N/A, groom lake/homey (KXTA) : 252.0
}
},
},
LandRWCategories =
{
[1] =
{
Name = "AircraftCarrier",
}, -- end of [1]
}, -- end of LandRWCategories
-- WingSpan = "8.38",--*
-- MaxFuelWeight = "2498.4",
-- MaxHeight = "12880",
-- MaxSpeed = "300",
-- MaxTakeOffWeight = "11136",
-- Picture = "A-4E.png",
-- Rate = "40",
-- Shape = "A-4E",
TakeOffRWCategories =
{
[1] =
{
Name = "AircraftCarrier With Catapult",
}, -- end of [1]
}, -- end of TakeOffRWCategories
WorldID = WSTYPE_PLACEHOLDER, -- A_4E,
Failures = {
{ id = 'asc', label = _('ASC'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'autopilot', label = _('AUTOPILOT'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'hydro', label = _('HYDRO'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'l_engine', label = _('L-ENGINE'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'r_engine', label = _('R-ENGINE'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'radar', label = _('RADAR'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'eos', label = _('EOS'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'helmet', label = _('HELMET'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
--{ id = 'mlws', label = _('MLWS'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'rws', label = _('RWS'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'ecm', label = _('ECM'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'hud', label = _('HUD'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
{ id = 'mfd', label = _('MFD'), enable = false, hh = 0, mm = 0, mmint = 1, prob = 100 },
},
-- Aircraft Additional Properties
AddPropAircraft = {
{
id = "HideECMPanel",
control = "checkbox",
label = _("Remove ECM control panel"),
defValue = false,
weightWhenOn = -80
},
{ id = "CBU2ATPP", control = 'comboList', label = _('CBU-2/A Tubes Per Pulse'),
values = {
{id = 0, dispName = _("1 tube")},
{id = 1, dispName = _("2 tubes")},
{id = 2, dispName = _("3 tubes")},
{id = 3, dispName = _("4 tubes")},
{id = 4, dispName = _("6 tubes")},
{id = 5, dispName = _("17 tubes (salvo)")},
},
defValue = 0,
wCtrl = 150,
playerOnly = true
},
{ id = "CBU2BATPP", control = 'comboList', label = _('CBU-2B/A Tubes Per Pulse'),
values = {
{id = 0, dispName = _("2 tubes")},
{id = 1, dispName = _("4 tubes")},
{id = 2, dispName = _("6 tubes")},
},
defValue = 0,
wCtrl = 150,
playerOnly = true
},
{ id = "CMS_BURSTS", control = 'comboList', label = _('CMS BURSTS'),
values = {
{id = 1, dispName = _("1")},
{id = 2, dispName = _("2")},
{id = 3, dispName = _("3")},
{id = 4, dispName = _("4")},
},
defValue = 1,
wCtrl = 150,
playerOnly = true
},
{ id = "CMS_BURST_INTERVAL", control = 'comboList', label = _('CMS BURST INTERVAL'),
values = {
{id = 1, dispName = _("0.2 seconds")},
{id = 2, dispName = _("0.3 seconds")},
{id = 3, dispName = _("0.4 seconds")},
{id = 4, dispName = _("0.5 seconds")},
},
defValue = 1,
wCtrl = 150,
playerOnly = true
},
{ id = "CMS_SALVOS", control = 'comboList', label = _('CMS SALVOS'),
values = {
{id = 1, dispName = _("8")},
{id = 2, dispName = _("12")},
{id = 3, dispName = _("16")},
{id = 4, dispName = _("20")},
{id = 5, dispName = _("24")},
{id = 6, dispName = _("28")},
{id = 7, dispName = _("32")},
},
defValue = 1,
wCtrl = 150,
playerOnly = true
},
{ id = "CMS_SALVO_INTERVAL", control = 'comboList', label = _('CMS SALVO INTERVAL'),
values = {
{id = 1, dispName = _("2 seconds")},
{id = 2, dispName = _("4 seconds")},
{id = 3, dispName = _("6 seconds")},
{id = 4, dispName = _("8 seconds")},
{id = 5, dispName = _("10 seconds")},
{id = 6, dispName = _("12 seconds")},
{id = 7, dispName = _("14 seconds")},
},
defValue = 1,
wCtrl = 150,
playerOnly = true
},
},
Guns = {
coltMK12({muzzle_pos_connector = "GUN_POINT_1",
rates = {1020},
--mixes = {{2,1,1,1,1,1}},
effect_arg_number = 434,
supply_position = {2, -0.3, -0.4},
ejector_pos_connector = "GUN_EJECT_1",
}),
coltMK12({muzzle_pos_connector = "GUN_POINT_2",
rates = {1020},
--mixes = {{2,1,1,1,1,1}},
effect_arg_number = 434,
supply_position = {2, -0.3, -0.4},
ejector_pos_connector = "GUN_EJECT_2",
}),
},
-- ammo_type = {
-- _("CM Combat Mix"),
-- _("HEI High Explosive Incendiary"),
-- _("TP Target Practice"),
-- },
Pylons = {
pylon(1, 0, -0.609, -0.762, -2.845, --
{
use_full_connector_position = true, connector = "Pylon1", arg = 341, arg_value = 0,
},
get_outboard_weapons("L")
),
pylon(2, 0, -0.047, -0.97, -1.899,
{
use_full_connector_position = true, connector = "Pylon2", arg = 342, arg_value = 0,
},
get_inboard_weapons("L")
),
pylon(3, 0, 0.11, -0.90, 0,
{
use_full_connector_position = true, connector = "Pylon3", arg = 343, arg_value = 0,
},
get_centerline_weapons("C")
),
pylon(4, 0, -0.047, -0.97, 1.899,
{
use_full_connector_position = true, connector = "Pylon4", arg = 344, arg_value = 0,
},
get_inboard_weapons("R")
),
pylon(5, 0, -0.609, -0.762, 2.845,
{
use_full_connector_position = true, connector = "Pylon5", arg = 345, arg_value = 0,
},
get_outboard_weapons("R")
),
},
Tasks = { -- defined in db_units_planes.lua, nothing is #15
aircraft_task(CAP), -- Task #11 in ME
aircraft_task(CAS), -- Task #31
aircraft_task(SEAD), -- Task #29
--aircraft_task(Reconnaissance),
aircraft_task(GroundAttack), -- Task #32
aircraft_task(AFAC), -- Task #16
--aircraft_task(RunwayAttack),
--aircraft_task(AntishipStrike),
aircraft_task(Refueling), -- Task #13
},
DefaultTask = aircraft_task(CAS),
SFM_Data = {
aerodynamics = -- Cx = Cx_0 + Cy^2*B2 +Cy^4*B4
{
Cy0 = 0.0, -- zero AoA lift coefficient
Mzalfa = 6.2, -- coefficients for pitch agility
Mzalfadt = 0.7, -- coefficients for pitch agility
kjx = 4.5, -- Inertia parametre X - Dimension (clean) airframe drag coefficient at X (Top) Simply the wing area in square meters (as that is a major factor in drag calculations) - smaller = massive inertia
kjz = 0.00125, -- Inertia parametre Z - Dimension (clean) airframe drag coefficient at Z (Front) Simply the wing area in square meters (as that is a major factor in drag calculations)
Czbe = -0.016, -- coefficient, along Z axis (perpendicular), affects yaw, negative value means force orientation in FC coordinate system
cx_gear = 0.07, -- coefficient, drag, gear ??
cx_flap = 0.08, -- coefficient, drag, full flaps -- 0.006 for first 10 degrees
cy_flap = 0.21, -- coefficient, normal force, lift, flaps -- 0.095 for first 10 degrees
cx_brk = 0.12, -- coefficient, drag speedbrake (0.04 for speedbrake, extra 0.08 to emulate the spoilers (see spoilers.lua and airbrakes.lua))
--[[ OLD table
table_data = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
{0.0, 0.012, 0.10, 0.04, 0.03, 0.5, 14, 1.0, },
{0.4, 0.0145, 0.10, 0.04, 0.03, 10.56, 14, 1.4, },
{0.5, 0.015, 0.09, 0.04, 0.03, 11.56, 14, 1.5, },
{0.6, 0.015, 0.08, 0.04, 0.03, 12.56, 14, 1.6, },
{0.7, 0.015, 0.07, 0.04, 0.03, 11.56, 14, 1.5, },
{0.8, 0.015, 0.06, 0.04, 0.03, 10.56, 14, 1.4, }, -- Cx0
{0.85, 0.015, 0.06, 0.04, 0.03, 9.56, 14, 1.4, }, -- 0.030
{0.9, 0.045, 0.05, 0.04, 0.03, 9.56, 14, 1.4, }, -- 0.060
}--]]
-- slat extension is automatic below 200 KCAS, linear to 100 KCAS
-- effect of slats is higher AoA possible, higher drag, higher lift
-- slat Cd at M0.6 is ~0.016 for 20 degree slat extension, with linear mapping
-- slat Cl at M0.6 is ~0.06/degree for 20 degree slat extension, 2/3 comes from the first 10 degrees
--[[
-- attempt #1 from naca report
table_data = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
{0.00, 0.0320, 0.066, 0.04, 0.03, 0.5, 14.50, 1.11, },
{0.15, 0.0320, 0.066, 0.04, 0.03, 10.56, 14.50, 1.11, }, -- 20 degree slat extension at sea level
{0.225, 0.0240, 0.064, 0.04, 0.03, 10.56, 12.50, 0.89, }, -- 10 degree slat extension at sea level
{0.30, 0.0160, 0.060, 0.04, 0.03, 10.56, 10.50, 0.77, }, -- 0 degree slat extension at sea level
{0.40, 0.0160, 0.060, 0.04, 0.03, 10.56, 10.30, 0.75, },
{0.50, 0.0160, 0.060, 0.04, 0.03, 11.56, 10.20, 0.73, },
{0.60, 0.0160, 0.060, 0.04, 0.03, 12.56, 10.10, 0.71, },
{0.70, 0.0163, 0.062, 0.04, 0.03, 11.56, 9.90, 0.68, },
{0.80, 0.0165, 0.066, 0.04, 0.03, 10.56, 8.75, 0.65, },
{0.85, 0.0180, 0.070, 0.04, 0.03, 9.56, 8.25, 0.60, },
{0.88, 0.0190, 0.078, 0.04, 0.03, 9.56, 8.25, 0.68, },
{0.9, 0.0200, 0.079, 0.04, 0.03, 9.56, 6.50, 0.72, },
{1.0, 0.0200, 0.073, 0.04, 0.03, 9.56, 6.50, 0.74, },
{1.1, 0.0200, 0.065, 0.04, 0.03, 9.56, 6.80, 0.74, },
}
--]]
-- now correcting for parasitic drag (drag index) -- roughly 1.5x at the top end to model a drag index of ~40 when empty
-- removed 10 degree slat line, was causing SFM interpolation bug
-- Cya max M0.15 of 0.95 results in approach noflap=137-140, fullflap=120-123 targets: 143/126 @ 14,000#
-- test: change Cya 0.96 -> 0.92 for M0.0 and M0.15, leave Cya 0.71 for M0.30, test at 14000#
-- result: 138-141 noflap, 121-123 flaps
-- test: Cya 0.92 -> 0.84 for M<=0.15, 0.71->0.66 M0.3, 14K#
-- result: 145-147 noflap, 126-127 flaps
-- test: Cya normalization 0.60 @ M0.40, 0.61 @ 0.30, 14K#
-- result: 145-147 noflap, 126-127 flaps
-- test: Cya 0.84->0.85 M<=0.15, 14K#
-- result: 144-147 noflap, 125-126 flaps close!
-- test: Cya 0.85->0.86, Cyflap 0.22->0.21, 14000#
-- result: 143-146 noflap, 126-127 flaps close for 14K#
-- test: Cya 0.86->0.87 M<=0.15
-- result: 142-145 noflap, 125-126 flaps done for 14K# (on target)
-- test: weight 12K#, target: 135/116.5
-- result: 131-133 noflap, 115-116 flaps done for 12K# (~2% too little lift w/o flaps)
-- test: weight 16K#, target: 153/134
-- result: 152-156 noflap, 134-135 flaps done for 16K# (on target)
--[[
table_data = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
{0.00, 0.0220, 0.087, 0.149, 0.00, 0.5, 13.15, 1.11, },
{0.15, 0.0220, 0.087, 0.149, 0.00, 1.0, 13.15, 1.11, }, -- 20 degree slat extension at sea level
{0.30, 0.0160, 0.061, 0.149, 0.00, 4.5, 11.50, 0.77, }, -- 0 degree slat extension at sea level
{0.40, 0.0160, 0.060, 0.149, 0.00, 6.5, 10.30, 0.75, },
{0.50, 0.0160, 0.060, 0.149, 0.00, 8.0, 10.20, 0.73, },
{0.60, 0.0160, 0.060, 0.149, 0.00, 8.1, 10.10, 0.71, },
{0.70, 0.0190, 0.062, 0.149, 0.00, 8.3, 9.90, 0.68, },
{0.80, 0.0200, 0.066, 0.149, 0.00, 8.3, 8.75, 0.65, },
{0.85, 0.0215, 0.070, 0.149, 0.00, 8.1, 8.25, 0.60, },
{0.88, 0.0245, 0.078, 0.169, 0.00, 7.8, 8.25, 0.68, },
{0.9, 0.0310, 0.079, 0.179, 0.00, 7.6, 6.50, 0.72, },
{1.0, 0.0350, 0.073, 0.352, 0.00, 7.6, 6.50, 0.74, },
{1.1, 0.0370, 0.065, 0.460, 0.00, 7.6, 6.80, 0.74, },
}
--]]
table_data = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
{0.00, 0.0220, 0.087, 0.149, 0.00, 0.5, 22.91, 1.40, },
{0.15, 0.0220, 0.087, 0.149, 0.00, 1.0, 22.91, 1.40, }, -- 20 degree slat extension at sea level
{0.30, 0.0160, 0.061, 0.149, 0.00, 4.5, 22.91, 1.30, }, -- 0 degree slat extension at sea level
{0.40, 0.0160, 0.060, 0.149, 0.00, 6.5, 22.91, 1.22, },
{0.48, 0.0160, 0.060, 0.149, 0.00, 7.5, 22.91, 1.05, },
{0.50, 0.0160, 0.060, 0.149, 0.00, 8.0, 22.34, 1.00, },
{0.55, 0.0160, 0.060, 0.149, 0.00, 8.0, 20.91, 0.96, },
{0.60, 0.0160, 0.060, 0.149, 0.00, 8.1, 18.33, 0.91, },
{0.65, 0.0175, 0.061, 0.149, 0.00, 8.2, 22.63, 0.89, },
{0.70, 0.0190, 0.062, 0.149, 0.00, 8.3, 25.21, 0.88, },
{0.80, 0.0200, 0.066, 0.149, 0.00, 8.3, 23.60, 0.86, },
{0.85, 0.0215, 0.070, 0.149, 0.00, 8.1, 21.77, 0.80, },
{0.88, 0.0245, 0.078, 0.169, 0.00, 7.8, 19.00, 0.76, },
{0.9, 0.0310, 0.079, 0.179, 0.00, 7.6, 18.33, 0.76, },
{0.95, 0.0335, 0.075, 0.280, 0.00, 7.6, 13.18, 0.76, },
{1.0, 0.0350, 0.073, 0.352, 0.00, 7.6, 10.30, 0.76, },
{1.1, 0.0370, 0.065, 0.460, 0.00, 7.6, 10.10, 0.76, },
}
-- M - Mach number
-- Cx0 - Coefficient, drag, profile, of the airplane
-- Cya - Normal force coefficient of the wing and body of the aircraft in the normal direction to that of flight. Inversely proportional to the available G-loading at any Mach value. (lower the Cya value, higher G available) per 1 degree AOA
-- B2 - Polar 2nd power coeff
-- B4 - Polar 4th power coeff
-- Omxmax - roll rate, rad/s
-- Aldop - Alfadop Max AOA at current M - departure threshold
-- Cymax - Coefficient, lift, maximum possible (ignores other calculations if current Cy > Cymax)
}, -- end of aerodynamics
engine =
{
Nmg = 55.0, -- RPM at idle
MinRUD = 0, -- Min state of the throttle
MaxRUD = 1, -- Max state of the throttle
MaksRUD = 0.999, -- Military power state of the throttle
ForsRUD = 0.99999, -- Afterburner state of the throttle
typeng = 0,
--[[
E_TURBOJET = 0
E_TURBOJET_AB = 1
E_PISTON = 2
E_TURBOPROP = 3
E_TURBOFAN = 4
E_TURBOSHAFT = 5
--]]
hMaxEng = 15, -- Max altitude for safe engine operation in km
dcx_eng = 0.0114, -- Engine drag coeficient
-- Affects drag of engine when shutdown
-- cemax/cefor affect sponginess of elevator/inertia at slow speed
-- affects available g load apparently
cemax = 0.037, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
cefor = 0.037, -- not used for fuel calulation , only for AI routines to check flight time ( fuel calculation algorithm is built in )
dpdh_m = 6000, -- altitude coefficient for max thrust
dpdh_f = 14000.0, -- altitude coefficient for AB thrust
table_data =
{
-- M Pmax
{0.0, 0.0,0.0}, -- dummy table, required for 2.0+ engine module load
{2.0, 0.0,0.0},
}, -- end of table_data
-- M - Mach number
-- Pmax - Engine thrust at military power - kilo Newton
-- Pfor - Engine thrust at AFB
extended = -- added new abilities for engine performance setup. thrust data now can be specified as 2d table by Mach number and altitude. thrust specific fuel consumption tuning added as well
{
-- matching TSFC to mil thrust consumption at altitude at mach per NATOPS navy trials
TSFC_max = -- thrust specific fuel consumption by altitude and Mach number for RPM 100%, 2d table
{
M = {0, 0.5, 0.8, 0.9, 1.0},
H = {0, 3048, 6096, 9144, 12192},
TSFC = {-- M 0 0.5 0.8 0.9 1.0
{ 0.86, 0.92, 1.012, 1.012, 1.003},--H = 0 -- SL
{ 0.86, 0.99, 1.025, 1.025, 1.016},--H = 3048 -- 10000'
{ 0.86, 0.96, 1.008, 1.008, 0.999},--H = 6096 -- 20000'
{ 0.86, 0.95, 0.984, 0.984, 0.974},--H = 9144 -- 30000'
{ 0.86, 0.94, 0.976, 0.976, 0.967},--H = 12192 -- 40000'
}
},
TSFC_afterburner = -- afterburning thrust specific fuel consumption by altitude and Mach number RPM 100%, 2d table
{
M = {0,0.3,0.5,0.7,1.0},
H = {0,1000,3000,10000},
TSFC = {-- M 0 0.3 0.5 0.7 1.0
{ 1, 1, 1, 1, 1},--H = 0
{ 1, 1, 1, 1, 1},--H = 1000
{ 1, 1, 1, 1, 1},--H = 3000
{ 1, 1, 1, 1, 1},--H = 10000
}
},
-- per ADA057325:
-- SFC = 0.836 (0% bleed) to 1.415 (15.44% bleed) at low throttle
-- SFC = 0.777 (0% bleed) to 0.964 (16.84% bleed) at MIL throttle
-- modeling as 5% bleed, so low power loses 22% efficiency:
TSFC_throttle_responce = -- correction to TSFC for different engine RPM, 1d table
{
RPM = {0, 50, 55, 75, 100},
K = {1, 1.05, 1.22, 1.05, 1.00}, -- Static SL TSFC now part of table above
--K = {1, 1, 1, 1, 1},
},
--[[
thrust_max = -- thrust interpolation table by altitude and mach number, 2d table
{
M = {0,.1,0.3,0.5,0.7,0.8,0.9,1.1},
H = {0,250,4572,7620,10668,13716,16764,19812},
thrust = {-- M 0 0.1 0.3 0.5 0.7 0.8 0.9 1.1
{ 61370, 59460, 57023, 36653, 36996, 37112, 36813, 34073 },--H = 0 (sea level)
{ 41370, 39460, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 250 (sea level)
{ 27254, 25799, 24203, 24599, 26227, 27254, 28353, 29785 },--H = 4572 (15kft)
{ 20818, 19203, 17548, 17473, 18638, 19608, 20684, 22873 },--H = 7620 (25kft)
{ 10876, 11076, 11556, 12193, 13024, 13674, 14434, 16098 },--H = 10668 (35kft)
{ 6025, 6379, 6837, 7433, 8194, 8603, 9101, 10075 },--H = 13716 (45kft)
{ 3336, 3554, 3990, 4484, 5000, 5307, 5596, 6232 },--H = 16764 (55kft)
{ 1904, 2042, 2433, 2798, 3212, 3483, 3639, 4097 },--H = 19812 (65kft)
},
},]]--
thrust_max = -- thrust interpolation table by altitude and mach number, 2d table. Modified for carrier takeoffs at/around 71 foot deck height
{
M = {0, 0.1, 0.225, 0.23, 0.3, 0.5, 0.7, 0.8, 0.9, 1.1},
H = {0, 19, 20, 23, 24, 250, 4572, 7620, 10668, 13716, 16764, 19812},
thrust = {-- M 0 0.1 0.225 0.23, 0.3 0.5 0.7 0.8 0.9 1.1
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 0 (sea level)
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 19 (~62.3 feet)
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 20 (~66.6 feet)
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 23 (~75.5 feet)
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 24 (~78.7 feet)
{ 41370, 39460, 38060, 38056, 37023, 36653, 36996, 37112, 36813, 34073 },--H = 250 (820 feet)
{ 27254, 25799, 24765, 24761, 24203, 24599, 26227, 27254, 28353, 29785 },--H = 4572 (15kft)
{ 20818, 19203, 18130, 18127, 17548, 17473, 18638, 19608, 20684, 22873 },--H = 7620 (25kft)
{ 10876, 11076, 11128, 11130, 11556, 12193, 13024, 13674, 14434, 16098 },--H = 10668 (35kft)
{ 6025, 6379, 6676, 6680, 6837, 7433, 8194, 8603, 9101, 10075 },--H = 13716 (45kft)
{ 3336, 3554, 3837, 3840, 3990, 4484, 5000, 5307, 5596, 6232 },--H = 16764 (55kft)
{ 1904, 2042, 2296, 2300, 2433, 2798, 3212, 3483, 3639, 4097 },--H = 19812 (65kft)
},
},
thrust_afterburner = -- afterburning thrust interpolation table by altitude and mach number, 2d table
{
M = {0, 0.20, 0.21, 1.0},
H = {0, 15, 16, 23, 24, 250, 19812},
thrust = { -- M 0 0.3 0.5 0.7 1.0
{ 41370, 41370, 41370, 41370,}, -- H = 0
{ 41370, 41370, 41370, 41370,}, -- H = 15
{ 250000, 250000, 41370, 41370,}, -- H = 16
{ 250000, 250000, 41370, 41370,}, -- H = 23
{ 41370, 38060, 38060, 36813,}, -- H = 24
{ 41370, 38060, 38060, 36813,}, -- H = 250
{ 1904, 2296, 2296, 3639,}, -- H= 19812
}
},
--rpm_acceleration_time_factor = -- time factor for engine governor ie RPM += (desired_RPM - RPM ) * t(RPM) * dt
--{
-- RPM = {0, 50, 100},
-- t = {0.3,0.3,0.3}
--},
--rpm_deceleration_time_factor = -- time factor for engine governor
--{
-- RPM = {0, 50, 100},
-- t = {0.3,0.3,0.3}
--},
rpm_throttle_responce = -- required RPM according to throttle position
{
throttle = {0 ,0.85 ,1.0},
RPM = {55 ,97.2 ,100},
},
thrust_rpm_responce = -- thrust = K(RPM) * thrust_max(M,H)
{
RPM = {0 ,55 ,55.1 ,57.6 ,65.8 ,74.1 ,78.2 ,82.3 ,90.5 ,98.8 ,100},
K = {0 ,0.00 ,0.051 ,0.059 ,0.101 ,0.176 ,0.248 ,0.349 ,0.670 ,0.963 ,1},
},
},
}, -- end of engine
},
--damage , index meaning see in Scripts\Aircrafts\_Common\Damage.lua
-- Damage = {
-- [0] = {critical_damage = 5, args = {82}}, -- 0 - nose center
-- [3] = {critical_damage = 10, args = {65}}, -- 3 - cockpit
-- [8] = {critical_damage = 10}, -- 8 - front gear
-- [11] = {critical_damage = 3}, -- 11 - engine in left
-- [12] = {critical_damage = 3}, -- 12 - engine in right
-- [15] = {critical_damage = 10}, -- 15 - gear left
-- [16] = {critical_damage = 10}, -- 16 - gear right
-- [17] = {critical_damage = 3}, -- 17 - motogondola left (left engine out, left ewu)
-- [18] = {critical_damage = 3}, -- 18 - motogondola right (right engine out, right ewu)
-- [25] = {critical_damage = 5, args = {53}}, -- 25 - eleron left
-- [26] = {critical_damage = 5, args = {54}}, -- 26 - eleron right
-- [35] = {critical_damage = 10, args = {67}, deps_cells = {25, 37}}, -- 35 - wing in left
-- [36] = {critical_damage = 10, args = {68}, deps_cells = {26, 38}}, -- 36 - wing in right
-- [37] = {critical_damage = 4, args = {55}}, -- 37 - flap in left
-- [38] = {critical_damage = 4, args = {56}}, -- 38 - flap in right
-- [43] = {critical_damage = 4, args = {61}, deps_cells = {53}}, -- 43 - fin bottom left
-- [44] = {critical_damage = 4, args = {62}, deps_cells = {54}}, -- 44 - fin bottom right
-- [47] = {critical_damage = 5, args = {63}, deps_cells = {51}}, -- 47 - stabilizer in left
-- [48] = {critical_damage = 5, args = {64}, deps_cells = {52}}, -- 48 - stabilizer in right
-- [51] = {critical_damage = 2, args = {59}}, -- 51 - elevator in left
-- [52] = {critical_damage = 2, args = {60}}, -- 52 - elevator in right
-- [53] = {critical_damage = 2, args = {57}}, -- 53 - rudder left
-- [54] = {critical_damage = 2, args = {58}}, -- 54 - rudder right
-- [55] = {critical_damage = 5, args = {81}}, -- 55 - tail
-- [83] = {critical_damage = 3, args = {134}}, -- nose wheel
-- [84] = {critical_damage = 3, args = {136}}, -- left wheel
-- [85] = {critical_damage = 3, args = {135}}, -- right wheel
-- },
Damage = verbose_to_dmg_properties(
{
["NOSE_CENTER"] = {critical_damage = 3}, -- 0
["NOSE_LEFT_SIDE"] = {critical_damage = 3}, -- 1
["NOSE_RIGHT_SIDE"] = {critical_damage = 3}, -- 2
["NOSE_BOTTOM"] = {critical_damage = 3}, -- 59
["COCKPIT"] = {critical_damage = 1}, -- 3
["CABIN_LEFT_SIDE"] = {critical_damage = 3}, -- 4
["CABIN_RIGHT_SIDE"] = {critical_damage = 3}, -- 5
["CABIN_BOTTOM"] = {critical_damage = 3}, -- 6
["GUN"] = {critical_damage = 2}, -- 7 refuelling probe?
["PITOT"] = {critical_damage = 1}, -- 60
["WHEEL_F"] = {critical_damage = 3}, -- 83
["FUSELAGE_LEFT_SIDE"] = {critical_damage = 3, args = {600}}, -- 9
["FUSELAGE_RIGHT_SIDE"] = {critical_damage = 3}, --10
["FUSELAGE_TOP"] = {critical_damage = 3}, -- 99 avionics hump?
["FUSELAGE_BOTTOM"] = {critical_damage = 4}, --82
["ENGINE"] = {critical_damage = 2},-- 11
-- ["MTG_L"] = {critical_damage = 3}, -- 17 left engine nacelle
-- ["MTG_R"] = {critical_damage = 3}, -- 18 right engine nacelle
["AIR_BRAKE_L"] = {critical_damage = 1}, -- 19
["AIR_BRAKE_R"] = {critical_damage = 1}, -- 20
["WING_L_IN"] = {critical_damage = 5, deps_cells = {"WING_L_CENTER"}}, -- 35
["WING_L_CENTER"] = {critical_damage = 4, deps_cells = {"WING_L_PART_CENTER", "FLAP_L", "WING_L_OUT"}}, -- 29
["WING_L_PART_CENTER"] = {critical_damage = 1.5}, -- 27 -- spoiler
["WING_L_OUT"] = {critical_damage = 3, deps_cells = {"AILERON_L"}}, -- 23
["FLAP_L"] = {critical_damage = 2}, -- 37
["AILERON_L"] = {critical_damage = 1}, --25
["WHEEL_L"] = {critical_damage = 3}, -- 84
["WING_R_IN"] = {critical_damage = 5, deps_cells = {"WING_R_CENTER"}}, -- 36
["WING_R_CENTER"] = {critical_damage = 4, deps_cells = {"WING_R_PART_CENTER", "FLAP_R", "WING_R_OUT"}}, -- 30
["WING_R_PART_CENTER"] = {critical_damage = 1.5}, -- 28 -- spoiler
["WING_R_OUT"] = {critical_damage = 3, deps_cells = {"AILERON_R"}}, -- 24
["FLAP_R"] = {critical_damage = 2}, -- 38
["AILERON_R"] = {critical_damage = 1}, --26
["WHEEL_R"] = {critical_damage = 3}, -- 85
["TAIL"] = {critical_damage = 2}, -- 55
["TAIL_LEFT_SIDE"] = {critical_damage = 3}, -- 56
["TAIL_RIGHT_SIDE"] = {critical_damage = 3}, -- 57
-- ["TAIL_BOTTOM"] = {critical_damage = 3}, --58
["STABILIZATOR_L"] = {critical_damage = 2, deps_cells = {"ELEVATOR_L"}}, -- 47
["ELEVATOR_L"] = {critical_damage = 1}, -- 51
["STABILIZATOR_R"] = {critical_damage = 2, deps_cells = {"ELEVATOR_R"}}, -- 48
["ELEVATOR_R"] = {critical_damage = 1}, -- 52
["RUDDER"] = {critical_damage = 1}, --53
["FIN_L_TOP"] = {critical_damage = 4}, --53
["FIN_L_BOTTOM"] = {critical_damage = 4, deps_cells = {"RUDDER", "FIN_L_TOP"}}, --53
-- ["HOOK"] = {critical_damage = 2}, -- 98
}),
DamageParts =
{
-- [1] = "a4_dmg_wing_right", -- Right Wing
-- [2] = "a4_dmg_wing_left", -- Left Wing
-- [3] = "a4_dmg_fus_front", -- nose
-- [4] = "a4_dmg_fus_back", -- tail
},
lights_data = {
typename = "collection",
lights = {
-- STROBES
[1] = {
typename = "collection",
lights = {
{typename = "argnatostrobelight", argument = 204, period = 1.2, phase_shift = 0},
{typename = "argnatostrobelight", argument = 205, period = 1.2, phase_shift = 0.5},
},
},
-- SPOTS / TAXI & LANDING
[2] = {
typename = "collection",
lights = { {typename = "argumentlight", argument = 208}, -- taxi light
},
},
-- NAVLIGHTS
[3] = {
typename = "collection",
lights = { {typename = "argumentlight", argument = 190}, -- red
{typename = "argumentlight", argument = 191}, -- green
{typename = "argumentlight", argument = 192}, -- white
},
},
-- FORMATION
[4] = {},
-- TIPS
[5] = {},
-- REFUEL
[6] = {
typename = "collection",
lights = { {typename = "argumentlight", argument = 193}, -- probe light
},
},
-- ANTI-COLLISION
[7] = {},
}, -- end of lights
}, -- end of lights_data
}
add_aircraft(A_4E_C)
from roblox-4.
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