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AIM-54A-MK47 vs AIM-54C-MK47

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local AIM_54A_Mk47 = {

local AIM_54C_Mk47 = {

category = CAT_AIR_TO_AIR,

name = "AIM_54A_Mk47",

name = "AIM_54C_Mk47",

user_name = _("AIM-54A-Mk47"),

user_name = _("AIM-54C-Mk47"),

wsTypeOfWeapon = {wsType_Weapon,wsType_Missile,wsType_AA_Missile,WSTYPE_PLACEHOLDER},

--class_name = "wAmmunitionPhoenix",

shape_table_data =

{

name = "AIM-54A_Mk47";

name = "AIM-54C";

file = "HB_F14_EXT_AIM54";

life = 1;

fire = { 0, 1};

username = "AIM-54A-Mk47";

username = "AIM-54C";

index = WSTYPE_PLACEHOLDER,

{

name = "HB_F14_EXT_PHX_ALU";

file = "HB_F14_EXT_PHX_ALU";

life = 1;

fire = { 0, 1};

index = WSTYPE_PLACEHOLDER,

Escort = 0,

Head_Type = 2,

sigma = {5, 5, 5},

M = 444.0,

M = 465.6,

H_max = 20000.0,

H_min = 1.0,

Diam = 380.0,

Cx_pil = 5,

D_max = 14000.0,

D_min = 700.0,

Head_Form = 1,

Life_Time = 160.0,

Nr_max = 18,

Nr_max = 21,

v_min = 140.0,

v_mid = 700.0,

Mach_max = 4.0,

t_b = 0.0,

t_acc = 3.0,

t_marsh = 5.0,

Range_max = 180000.0,

H_min_t = 3.0,

Fi_start = 0.5,

Fi_rak = 3.14152,

Fi_excort = 1.05,

Fi_search = 1.05,

OmViz_max = 0.52,

warhead = warheads["AIM_54"],

exhaust = { 1, 1, 1, 1 }, -- smoke "high"

exhaust = {0.8, 0.8, 0.8, 0.05 }; -- smoke "none"

X_back = -1.72,

Y_back = 0.0,

Z_back = 0.0,

Reflection = 0.12,

KillDistance = 15.0,

ccm_k0 = 0.3,

ccm_k0 = 0.25,

loft = 0,

hoj = 0,

go_active_by_default = 0,

active_radar_lock_dist = 18520,

KillDistance = 15.0,

loft = 1,

hoj = 1,

PN_coeffs = {11, -- Number of Entries

0.0, 1.0,

4000.0, 0.995,

5000.0, 0.99,

6000.0, 0.97,

7000.0, 0.94,

10000.0, 0.80,

15000.0, 0.50,

20000.0, 0.35,

30000.0, 0.20,

40000.0, 0.14,

100000.0, 0.05,

};

ModelData = { 58, -- model params count

0.9, -- characteristic square (ÑÐ°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸ÑÐµÑÐºÐ°Ð¯ Ð¿Ð»Ð¾ÑÐ°Ð´Ñ)

-- Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð·Ð°Ð²Ð¸ÑÐ¸Ð¼Ð¾ÑÑÐ¸ âx

0.01, -- Cx_k0 Ð¿Ð»Ð°Ð½ÐºÐ° âx0 Ð½Ð° Ð´Ð¾Ð·Ð²ÑÐºÐµ ( M << 1)

0.028, -- Cx_k3 Ð¿Ð»Ð°Ð½ÐºÐ° Cx0 Ð½Ð° ÑÐ²ÐµÑÑÐ·Ð²ÑÐºÐµ ( M >> 1)

-- Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð·Ð°Ð²Ð¸ÑÐ¸Ð¼Ð¾ÑÑÐ¸ Cy

0.9, -- Cy_k0 Ð¿Ð»Ð°Ð½ÐºÐ° ây0 Ð½Ð° Ð´Ð¾Ð·Ð²ÑÐºÐµ ( M << 1)

0.8, -- Cy_k1 Ð¿Ð»Ð°Ð½ÐºÐ° Cy0 Ð½Ð° ÑÐ²ÐµÑÑÐ·Ð²ÑÐºÐµ ( M >> 1)

-- Engine data. Time, fuel flow, thrust.

-- t_statr t_b t_accel t_march t_inertial t_break t_end -- Stage

-- t_start t_b t_accel t_march t_inertial t_break t_end -- Stage

0.27, -1.0, 27.0, 0.0, 0.0, 0.0, 1.0e9, -- time of stage, sec

0.0, 0.0, 6.32, 0.0, 0.0, 0.0, 0.0, -- fuel flow rate in second, kg/sec(ÑÐµÐºÑÐ½Ð´Ð½ÑÐ¹ ÑÐ°ÑÑÐ¾Ð´ Ð¼Ð°ÑÑÑ ÑÐ¾Ð¿Ð»Ð¸Ð²Ð° ÐºÐ³/ÑÐµÐº)

0.0, 0.0, 6.048, 0.0, 0.0, 0.0, 0.0, -- fuel flow rate in second, kg/sec(ÑÐµÐºÑÐ½Ð´Ð½ÑÐ¹ ÑÐ°ÑÑÐ¾Ð´ Ð¼Ð°ÑÑÑ ÑÐ¾Ð¿Ð»Ð¸Ð²Ð° ÐºÐ³/ÑÐµÐº)

0.0, 0.0, 15982.0, 0.0, 0.0, 0.0, 0.0, -- thrust, newtons

0.0, 0.0, 15723.1, 0.0, 0.0, 0.0, 0.0, -- thrust, newtons

3.2,

70.0, -- ÑÐ°ÑÑÐµÑ Ð²ÑÐµÐ¼ÐµÐ½Ð¸ Ð¿Ð¾Ð»ÐµÑÐ°

63000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ 180(Ð½Ð°Ð²ÑÑÑÐµÑÑ) Ð³ÑÐ°Ð´, Ð=10000Ð¼, V=900ÐºÐ¼/Ñ, Ð¼

25000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ 0(Ð² Ð´Ð¾Ð³Ð¾Ð½) Ð³ÑÐ°Ð´, Ð=10000Ð¼, V=900ÐºÐ¼/Ñ

22000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ 180(Ð½Ð°Ð²ÑÑÑÐµÑÑ) Ð³ÑÐ°Ð´, Ð=1000Ð¼, V=900ÐºÐ¼/Ñ

0.2,

0.6,

1.4,

-3.0,

0.5,

}

declare_weapon(AIM_54A_Mk47)

declare_weapon(AIM_54C_Mk47)

Diff salvati

Testo originale

Apri file

local AIM_54A_Mk47 = {
    category		= CAT_AIR_TO_AIR,
    name			= "AIM_54A_Mk47",
    user_name		= _("AIM-54A-Mk47"),
    wsTypeOfWeapon 	= {wsType_Weapon,wsType_Missile,wsType_AA_Missile,WSTYPE_PLACEHOLDER},
    --class_name	= "wAmmunitionPhoenix",
    shape_table_data =
    {
        {
            name	 = "AIM-54A_Mk47";
            file  = "HB_F14_EXT_AIM54";
            life  = 1;
            fire  = { 0, 1};
            username = "AIM-54A-Mk47";
            index = WSTYPE_PLACEHOLDER,
        },
        {
            name = "HB_F14_EXT_PHX_ALU";
            file = "HB_F14_EXT_PHX_ALU";
            life = 1;
            fire = { 0, 1};
            index = WSTYPE_PLACEHOLDER,
        },
    },

Escort = 0,
        Head_Type = 2,
        sigma = {5, 5, 5},
        M = 444.0,
        H_max = 20000.0,
        H_min = 1.0,
        Diam = 380.0,
        Cx_pil = 5,
        D_max = 14000.0,
        D_min = 700.0,
        Head_Form = 1,
        Life_Time = 160.0,
        Nr_max = 18,
        v_min = 140.0,
        v_mid = 700.0,
        Mach_max = 4.0,
        t_b = 0.0,
        t_acc = 3.0,
        t_marsh = 5.0,
        Range_max = 180000.0,
        H_min_t = 3.0,
        Fi_start = 0.5,
        Fi_rak = 3.14152,
        Fi_excort = 1.05,
        Fi_search = 1.05,
        OmViz_max = 0.52,
        warhead = warheads["AIM_54"],
        exhaust = { 1, 1, 1, 1 },  -- smoke "high"
        X_back = -1.72,
        Y_back = 0.0,
        Z_back = 0.0,
        Reflection = 0.12,
        KillDistance = 15.0,
		ccm_k0 = 0.3,
        loft = 0,
        hoj = 0,
        go_active_by_default = 0,
        active_radar_lock_dist = 18520,
		
        PN_coeffs = {11,                 -- Number of Entries
                    0.0, 1.0,
                    4000.0, 0.995,
                    5000.0, 0.99,
                    6000.0, 0.97,
                    7000.0, 0.94,
                    10000.0, 0.80,
                    15000.0, 0.50,
                    20000.0, 0.35,
                    30000.0, 0.20,
                    40000.0, 0.14,
                    100000.0, 0.05,
                    };

ModelData = {   58,  -- model params count
                        0.9,   -- characteristic square (ÑÐ°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸ÑÐµÑÐºÐ°Ð¯ Ð¿Ð»Ð¾ÑÐ°Ð´Ñ)

-- Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð·Ð°Ð²Ð¸ÑÐ¸Ð¼Ð¾ÑÑÐ¸ âx
                        0.01, -- Cx_k0 Ð¿Ð»Ð°Ð½ÐºÐ° âx0 Ð½Ð° Ð´Ð¾Ð·Ð²ÑÐºÐµ ( M << 1)
                        0.031, -- Cx_k1 Ð²ÑÑÐ¾ÑÐ° Ð¿Ð¸ÐºÐ° Ð²Ð¾Ð»Ð½Ð¾Ð²Ð¾Ð³Ð¾ ÐºÑÐ¸Ð·Ð¸ÑÐ°
                        0.03, -- Cx_k2 ÐºÑÑÑÐ¸Ð·Ð½Ð° ÑÑÐ¾Ð½ÑÐ° Ð½Ð° Ð¿Ð¾Ð´ÑÐ¾Ð´Ðµ Ðº Ð²Ð¾Ð»Ð½Ð¾Ð²Ð¾Ð¼Ñ ÐºÑÐ¸Ð·Ð¸ÑÑ
                        0.028, -- Cx_k3 Ð¿Ð»Ð°Ð½ÐºÐ° Cx0 Ð½Ð° ÑÐ²ÐµÑÑÐ·Ð²ÑÐºÐµ ( M >> 1)
                        0.9, -- Cx_k4 ÐºÑÑÑÐ¸Ð·Ð½Ð° ÑÐ¿Ð°Ð´Ð° Ð·Ð° Ð²Ð¾Ð»Ð½Ð¾Ð²ÑÐ¼ ÐºÑÐ¸Ð·Ð¸ÑÐ¾Ð¼
                        1.5, -- ÐºÐ¾ÑÑÑÐ¸ÑÐ¸ÐµÐ½Ñ Ð¾ÑÐ²Ð°Ð»Ð° Ð¿Ð¾Ð»Ð¯ÑÑ (Ð¿ÑÐ¾Ð¿Ð¾ÑÑÐ¸Ð¾Ð½Ð°Ð»ÑÐ½Ð¾ sqrt (M^2-1))

-- Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ Ð·Ð°Ð²Ð¸ÑÐ¸Ð¼Ð¾ÑÑÐ¸ Cy
                        0.9, -- Cy_k0 Ð¿Ð»Ð°Ð½ÐºÐ° ây0 Ð½Ð° Ð´Ð¾Ð·Ð²ÑÐºÐµ ( M << 1)
                        0.8, -- Cy_k1 Ð¿Ð»Ð°Ð½ÐºÐ° Cy0 Ð½Ð° ÑÐ²ÐµÑÑÐ·Ð²ÑÐºÐµ ( M >> 1)
                        1.2, -- Cy_k2 ÐºÑÑÑÐ¸Ð·Ð½Ð° ÑÐ¿Ð°Ð´Ð°(ÑÑÐ¾Ð½ÑÐ°) Ð·Ð° Ð²Ð¾Ð»Ð½Ð¾Ð²ÑÐ¼ ÐºÑÐ¸Ð·Ð¸ÑÐ¾Ð¼

-- Engine data. Time, fuel flow, thrust.
                    --  t_statr     t_b     t_accel     t_march     t_inertial      t_break     t_end           -- Stage
                         0.27,       -1.0,   27.0,       0.0,        0.0,            0.0,        1.0e9,         -- time of stage, sec
                         0.0,       0.0,    6.32,       0.0,        0.0,            0.0,        0.0,           -- fuel flow rate in second, kg/sec(ÑÐµÐºÑÐ½Ð´Ð½ÑÐ¹ ÑÐ°ÑÑÐ¾Ð´ Ð¼Ð°ÑÑÑ ÑÐ¾Ð¿Ð»Ð¸Ð²Ð° ÐºÐ³/ÑÐµÐº)
                         0.0,       0.0,    15982.0,    0.0,        0.0,            0.0,        0.0,           -- thrust, newtons

1.0e9, -- ÑÐ°Ð¹Ð¼ÐµÑ ÑÐ°Ð¼Ð¾Ð»Ð¸ÐºÐ²Ð¸Ð´Ð°ÑÐ¸Ð¸, ÑÐµÐº
                         160.0, -- Ð²ÑÐµÐ¼Ð¯ ÑÐ°Ð±Ð¾ÑÑ ÑÐ½ÐµÑÐ³Ð¾ÑÐ¸ÑÑÐµÐ¼Ñ, ÑÐµÐº
                         0, -- Ð°Ð±ÑÐ¾Ð»ÑÑÐ½Ð°Ð¯ Ð²ÑÑÐ¾ÑÐ° ÑÐ°Ð¼Ð¾Ð»Ð¸ÐºÐ²Ð¸Ð´Ð°ÑÐ¸Ð¸, Ð¼
                         1.5, -- Ð²ÑÐµÐ¼Ð¯ Ð·Ð°Ð´ÐµÑÐ¶ÐºÐ¸ Ð²ÐºÐ»ÑÑÐµÐ½Ð¸Ð¯ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ð¯ (Ð¼Ð°Ð½ÐµÐ²Ñ Ð¾ÑÐ»ÐµÑÐ°, Ð±ÐµÐ·Ð¾Ð¿Ð°ÑÐ½Ð¾ÑÑÐ¸), ÑÐµÐº
                         30000, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ Ð´Ð¾ ÑÐµÐ»Ð¸ Ð² Ð¼Ð¾Ð¼ÐµÐ½Ñ Ð¿ÑÑÐºÐ°, Ð¿ÑÐ¸ Ð¿ÑÐµÐ²ÑÑÐµÐ½Ð¸Ð¸ ÐºÐ¾ÑÐ¾ÑÐ¾Ð¹ ÑÐ°ÐºÐµÑÐ° Ð²ÑÐ¿Ð¾Ð»Ð½Ð¯ÐµÑÑÐ¯ Ð¼Ð°Ð½ÐµÐ²Ñ "Ð³Ð¾ÑÐºÐ°", Ð¼
                         40000, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ Ð´Ð¾ ÑÐµÐ»Ð¸, Ð¿ÑÐ¸ ÐºÐ¾ÑÐ¾ÑÐ¾Ð¹ Ð¼Ð°Ð½ÐµÐ²Ñ "Ð³Ð¾ÑÐºÐ°" Ð·Ð°Ð²ÐµÑÑÐ°ÐµÑÑÐ¯ Ð¸ ÑÐ°ÐºÐµÑÐ° Ð¿ÐµÑÐµÑÐ¾Ð´Ð¸Ñ Ð½Ð° ÑÐ¸ÑÑÑÑ Ð¿ÑÐ¾Ð¿Ð¾ÑÑÐ¸Ð¾Ð½Ð°Ð»ÑÐ½ÑÑ Ð½Ð°Ð²Ð¸Ð³Ð°ÑÐ¸Ñ (Ð´Ð¾Ð»Ð¶ÐµÐ½ Ð±ÑÑÑ Ð±Ð¾Ð»ÑÑÐµ Ð¸Ð»Ð¸ ÑÐ°Ð²ÐµÐ½ Ð¿ÑÐµÐ´ÑÐ´ÑÑÐµÐ¼Ñ Ð¿Ð°ÑÐ°Ð¼ÐµÑÑÑ), Ð¼
                         0.20,  -- ÑÐ¸Ð½ÑÑ ÑÐ³Ð»Ð° Ð²Ð¾Ð·Ð²ÑÑÐµÐ½Ð¸Ð¯ ÑÑÐ°ÐµÐºÑÐ¾ÑÐ¸Ð¸ Ð½Ð°Ð±Ð¾ÑÐ° Ð³Ð¾ÑÐºÐ¸
                         50.0, -- Ð¿ÑÐ¾Ð´Ð¾Ð»ÑÐ½Ð¾Ðµ ÑÑÐºÐ¾ÑÐµÐ½Ð¸Ð¯ Ð²Ð·Ð²ÐµÐ´ÐµÐ½Ð¸Ð¯ Ð²Ð·ÑÑÐ²Ð°ÑÐµÐ»Ð¯
                         0.0, -- Ð¼Ð¾Ð´ÑÐ»Ñ ÑÐºÐ¾ÑÐ¾ÑÑÐ¸ ÑÐ¾Ð¾Ð±ÑÐ°Ð¹Ð¼ÑÐ¹ ÐºÐ°ÑÐ°Ð¿ÑÐ»ÑÑÐ½ÑÐ¼ ÑÑÑÑÐ¾Ð¹ÑÑÐ²Ð¾Ð¼, Ð²ÑÑÐ¸Ð±Ð½ÑÐ¼ Ð·Ð°ÑÐ¯Ð´Ð¾Ð¼ Ð¸ ÑÐ´
                         1.19, -- ÑÐ°ÑÐ°ÐºÑÑÐ¸ÑÑÐ¸ÐºÐ° ÑÐ¸ÑÑÐµÐ¼Ñ âÐâ-ÑÐÐâ¦âÐ,  ÐºÐ¾ÑÑ ÑÐ¸Ð»ÑÑÑÐ° Ð²ÑÐ¾ÑÐ¾Ð³Ð¾ Ð¿Ð¾ÑÐ¯Ð´ÐºÐ° K0
                         1.0, -- ÑÐ°ÑÐ°ÐºÑÑÐ¸ÑÑÐ¸ÐºÐ° ÑÐ¸ÑÑÐµÐ¼Ñ âÐâ-ÑÐÐâ¦âÐ,  ÐºÐ¾ÑÑ ÑÐ¸Ð»ÑÑÑÐ° Ð²ÑÐ¾ÑÐ¾Ð³Ð¾ Ð¿Ð¾ÑÐ¯Ð´ÐºÐ° K1
                         2.0, -- ÑÐ°ÑÐ°ÐºÑÑÐ¸ÑÑÐ¸ÐºÐ° ÑÐ¸ÑÑÐµÐ¼Ñ âÐâ-ÑÐÐâ¦âÐ,  Ð¿Ð¾Ð»Ð¾ÑÐ° Ð¿ÑÐ¾Ð¿ÑÑÐºÐ°Ð½Ð¸Ð¯ ÐºÐ¾Ð½ÑÑÑÐ° ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ð¯
                         25200.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ Ð¿Ð¾Ð»ÐµÑÐ° Ð² Ð³Ð¾ÑÐ¸Ð·Ð¾Ð½Ñ Ñ ÑÐ°ÑÐ¿Ð¾Ð»Ð°Ð³Ð°ÐµÐ¼Ð¾Ð¹ Ð¿ÐµÑÐµÐ³ÑÑÐ·ÐºÐ¾Ð¹ Navail >= 1.0 Ð½Ð° Ð²ÑÑÐ¾ÑÐµ H=2000
                         3.92, -- ÐºÑÑÑÐ¸Ð·Ð½Ð° Ð·Ð°Ð²Ð¸ÑÐ¸Ð¼Ð¾ÑÑÐ¸  Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ Ð¿Ð¾Ð»ÐµÑÐ° Ð² Ð³Ð¾ÑÐ¸Ð·Ð¾Ð½Ñ Ñ ÑÐ°ÑÐ¿Ð¾Ð»Ð°Ð³Ð°ÐµÐ¼Ð¾Ð¹ Ð¿ÐµÑÐµÐ³ÑÑÐ·ÐºÐ¾Ð¹ Navail >= 1.0 Ð¾Ñ Ð²ÑÑÐ¾ÑÑ H
                         3.2,
                         0.75, -- Ð±ÐµÐ·ÑÐ°Ð·Ð¼ÐµÑÐ½ÑÐ¹ ÐºÐ¾ÑÑ. ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾ÑÑÐ¸ âÐâ ÑÐ°ÐºÐµÑÑ
                         70.0, -- ÑÐ°ÑÑÐµÑ Ð²ÑÐµÐ¼ÐµÐ½Ð¸ Ð¿Ð¾Ð»ÐµÑÐ°
                          -- DLZ. âÐ°Ð½Ð½ÑÐµ Ð´Ð»Ð¯ ÑÐ°ÑÑÑÐµÑÐ° Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÐµÐ¹ Ð¿ÑÑÐºÐ° (Ð¸Ð½Ð´Ð¸ÐºÐ°ÑÐ¸Ð¯ Ð½Ð° Ð¿ÑÐ¸ÑÐµÐ»Ðµ)
                         63000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ   180(Ð½Ð°Ð²ÑÑÑÐµÑÑ) Ð³ÑÐ°Ð´,  Ð=10000Ð¼, V=900ÐºÐ¼/Ñ, Ð¼
                         25000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ 0(Ð² Ð´Ð¾Ð³Ð¾Ð½) Ð³ÑÐ°Ð´,  Ð=10000Ð¼, V=900ÐºÐ¼/Ñ
                         22000.0, -- Ð´Ð°Ð»ÑÐ½Ð¾ÑÑÑ ÑÐ°ÐºÑÑÑ    180(Ð½Ð°Ð²ÑÑÑÐµÑÑ) Ð³ÑÐ°Ð´, Ð=1000Ð¼, V=900ÐºÐ¼/Ñ
                         0.2,
                         0.6,
                         1.4,
                        -3.0,
                        0.5,
                    },
    }
declare_weapon(AIM_54A_Mk47)

Testo modificato

Apri file

local AIM_54C_Mk47 = {
    category		= CAT_AIR_TO_AIR,
    name			= "AIM_54C_Mk47",
    user_name		= _("AIM-54C-Mk47"),
    wsTypeOfWeapon 	= {wsType_Weapon,wsType_Missile,wsType_AA_Missile,WSTYPE_PLACEHOLDER},

shape_table_data =
    {
        {
            name	 = "AIM-54C";
            file  = "HB_F14_EXT_AIM54";
            life  = 1;
            fire  = { 0, 1};
            username = "AIM-54C";
            index = WSTYPE_PLACEHOLDER,
        },
    },

Escort = 0,
        Head_Type = 2,
        sigma = {5, 5, 5},
        M = 465.6,
        H_max = 20000.0,
        H_min = 1.0,
        Diam = 380.0,
        Cx_pil = 5,
        D_max = 14000.0,
        D_min = 700.0,
        Head_Form = 1,
        Life_Time = 160.0,
        Nr_max = 21,
        v_min = 140.0,
        v_mid = 700.0,
        Mach_max = 4.0,
        t_b = 0.0,
        t_acc = 3.0,
        t_marsh = 5.0,
        Range_max = 180000.0,
        H_min_t = 3.0,
        Fi_start = 0.5,
        Fi_rak = 3.14152,
        Fi_excort = 1.05,
        Fi_search = 1.05,
        OmViz_max = 0.52,
        warhead = warheads["AIM_54"],
        exhaust = {0.8, 0.8, 0.8, 0.05 }; -- smoke "none"
        X_back = -1.72,
        Y_back = 0.0,
        Z_back = 0.0,
        Reflection = 0.12,
        KillDistance = 15.0,
        ccm_k0 = 0.25,
        loft = 0,
        hoj = 0,
        go_active_by_default = 0,
        active_radar_lock_dist = 18520,
        KillDistance = 15.0,
        loft = 1,
        hoj = 1,

PN_coeffs = {11,                 -- Number of Entries
                    0.0, 1.0,
                    4000.0, 0.995,
                    5000.0, 0.99,
                    6000.0, 0.97,
                    7000.0, 0.94,
                    10000.0, 0.80,
                    15000.0, 0.50,
                    20000.0, 0.35,
                    30000.0, 0.20,
                    40000.0, 0.14,
                    100000.0, 0.05,
                    };

ModelData = {   58,  -- model params count
                        0.9,   -- characteristic square (ÑÐ°ÑÐ°ÐºÑÐµÑÐ¸ÑÑÐ¸ÑÐµÑÐºÐ°Ð¯ Ð¿Ð»Ð¾ÑÐ°Ð´Ñ)

-- Engine data. Time, fuel flow, thrust.
                    --  t_start     t_b     t_accel     t_march     t_inertial      t_break     t_end           -- Stage
                         0.27,       -1.0,   27.0,       0.0,        0.0,            0.0,        1.0e9,         -- time of stage, sec
                         0.0,       0.0,    6.048,      0.0,        0.0,            0.0,        0.0,           -- fuel flow rate in second, kg/sec(ÑÐµÐºÑÐ½Ð´Ð½ÑÐ¹ ÑÐ°ÑÑÐ¾Ð´ Ð¼Ð°ÑÑÑ ÑÐ¾Ð¿Ð»Ð¸Ð²Ð° ÐºÐ³/ÑÐµÐº)
                         0.0,       0.0,    15723.1,    0.0,        0.0,            0.0,        0.0,           -- thrust, newtons