[fltsim.0]
title=PZL M-15 Belphegor Aeroflot
sim=PZL M-15 Belphegor
model=
panel=
sound=
texture=
kb_checklists=

atc_id=15154
ui_manufacturer=PZL
ui_type=M-15 Belphegor
ui_variation=Aeroflot
atc_airline=Aeroflot
atc_flight_number=
atc_heavy=0
description=Of unusual configuration, the M-15 had unequal-span biplane wings, twin tailbooms extending aft to twin fins and rudders united by a high-set tailplane and elevator, and fixed tricycle landing gear. A central fuselage nacelle provided accommodation for the pilot and, to his rear, had a cabin to seat two ground crew during ferry flights between operating areas. The single turbofan power-plant was mounted above the fuselage nacelle, and two streamlined chemical hoppers occupied the full gap between each wing, mounted directly beneath the tailbooms, their combined chemical capacity 2900 litres.    Plans had been made to manufacture 3,000 M-15s, which had been given the name Belphegor during 1979, but production ended in 1981 after only 120 had been built because the aircraft was uneconomical in operation, P.Z.L. producing the turboprop An-3 instead.

[General]
atc_type= 
atc_model= 
editable=1 
performance="Weights: Maximum take-off weight 5750 kg 12677 lbs.\nDIMENSIONS: Wingspan 22.33 m 73 ft 3 in\nLength 13.13 m 43 ft 1 in\nHeight 5.34 m 17 ft 6 in\nWing area 67.9 m2 730.87 sq ft\nPERFORMANCE: Max. speed 200 km/h 124 mph\nCruise speed 175 km/h 109 mph\nRange 480 km 298 miles 



[weight_and_balance]

// ACM V2.5
max_gross_weight =11684.0
empty_weight =5291.00000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.000, 0.000, 0.000
empty_weight_pitch_MOI =12374.90000
empty_weight_roll_MOI =14659.52000
empty_weight_yaw_MOI =24334.27000
empty_weight_coupled_MOI =0.00000
max_number_of_stations =2
station_load.0= 170, 10.990, 0.000, 0.100
station_load.1= 170, 8.390, 0.000, 0.100




[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing

light.0 = 2, -0.25, -36.84, 7.83, fx_strobe
light.1 = 2, -0.25, 36.84, 7.83, fx_strobe
light.2 = 4, 5.54, 0, 0, fx_vclight
light.3 = 9, -4.02, 0, 3.06, fx_262_smoke_rx
light.4 = 10, 9.71, 0, 0, fx_vclight


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type =1
fuel_flow_scalar =1.12000
min_throttle_limit =0.00000
engine.0 =-4.050, 0.000, 3.070


[smokesystem]
smoke.0 = -5, 0, -25, fx_thrush_spray_tip_minus
smoke.1 = -5, 0, 1.04, fx_thrush_spray
smoke.2 = -5, 0, -24.69, fx_thrush_spray
smoke.3 = -5, 0, -23.51, fx_thrush_spray
smoke.4 = -5, 0, -14.25, fx_thrush_spray
smoke.5 = -5, 0, -11.38, fx_thrush_spray
smoke.6 = -5, 0, -22.61, fx_thrush_spray
smoke.7 = -5, 0, -12.87, fx_thrush_spray
smoke.8 = -5, 0, 12.8, fx_thrush_spray
smoke.9 = -5, 0, 22.26, fx_thrush_spray
smoke.10 = -5, 0, 11.52, fx_thrush_spray
smoke.11 = -5, 0, 13.83, fx_thrush_spray
smoke.12 = -5, 0, 23.44, fx_thrush_spray
smoke.13 = -5, 0, 24.9, fx_thrush_spray
smoke.14 = -5, 0, 25, fx_thrush_spray_tip_plus


[effects]
wake = fx_wake
water = fx_spray
dirt = fx_nicksjp_tchdirt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_vega
windshield_rain_effect_available = 1


[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type =2
number_of_tank_selectors =1
electric_pump =1

LeftMain = -2.000, -4.000, 2.000, 385.000, 3.600
RightMain = -2.000, 4.000, 2.000, 385.000, 3.600
fuel_dump_rate=0.02000
anemometer_pump=0
engine_driven_pump=0
manual_pump=0



[contact_points]
static_pitch = 0.000
static_cg_height = 6.950
tailwheel_lock =0
gear_system_type =0
max_number_of_points =9
point.0= 1, 14.500, 0.000, -6.100, 1500, 0, 0.900, 50.000, 0.200, 3.750, 0.700, 0.000, 0.000, 0
point.1= 1, -1.250, -7.250, -6.725, 2500, 1, 1.200, 0.000, 0.410, 1.829, 0.700, 0.000, 0.000, 2
point.2= 1, -1.250, 7.250, -6.725, 2500, 2, 1.200, 0.000, 0.410, 1.829, 0.700, 0.000, 0.000, 3
point.3= 2, 0.000, -26.500, -1.992, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, 0.000, 26.500, -1.992, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -19.599, 8.590, 0.620, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, -19.599, 8.590, 0.620, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.7= 2, -19.599, -8.590, 0.620, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.8= 2, 13.596, 0.000, -3.051, 3000, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4




[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000



[forcefeedback]
gear_bump_nose_magnitude =6000
gear_bump_nose_direction =18000
gear_bump_nose_duration =250000
gear_bump_left_magnitude =6000
gear_bump_left_direction =35500
gear_bump_left_duration =250000
gear_bump_right_magnitude =6000
gear_bump_right_direction =500
gear_bump_right_duration =250000
ground_bumps_magnitude1 =3250
ground_bumps_angle1 =8900
ground_bumps_intercept1 =5
ground_bumps_slope1 =0.48
ground_bumps_magnitude2 =750
ground_bumps_angle2 =9100
ground_bumps_intercept2 =0.075
ground_bumps_slope2 =1
crash_magnitude1 =10000
crash_direction1 =1000
crash_magnitude2 =10000
crash_direction2 =9000
crash_period2 =75000
crash_duration2 =2500000
stick_shaker_magnitude =5000
stick_shaker_direction =0
stick_shaker_period =111111


[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.1335,0.8822,0.8822,0,2.0269,1.7644,1.7644
//ACM_AREAW2// 0,1.9198,2.6466,2.6466,0,1.8135,3.5288,3.5288,0,1.7065
//ACM_AREAW3// 4.4109,4.4109,0,1.6002,5.2933,5.2933,0,1.4931,6.1753,6.1753
//ACM_AREAW4// 0,1.3868,7.0577,7.0577,0,1.2798,7.9400,7.9400,0,1.1734
//ACM_AREAH1// 0,0,0,1.1885,0.1981,0.1981,0.0173,1.1466,0.3962,0.3962
//ACM_AREAH2// 0.0346,1.1045,0.5942,0.5942,0.0518,1.0621,0.7924,0.7924,0.0693,1.0203
//ACM_AREAH3// 0.9904,0.9904,0.0864,0.9782,1.1885,1.1885,0.1039,0.9361,1.3868,1.3868
//ACM_AREAH4// 0.1212,0.8938,1.5849,1.5849,0.1386,0.8518,1.7826,1.7826,0.1559,0.8097
//ACM_AREAV1// 0,0,0,1.4630,0.1624,0.1624,0.1624,1.5082,0.3251,0.3251
//ACM_AREAV2// 0.3251,1.5540,0.4875,0.4875,0.4875,1.5994,0.6502,0.6502,0.6502,1.6447
//ACM_AREAV3// 0.8126,0.8126,0.8126,1.6906,0.9753,0.9753,0.9753,1.7359,1.1375,1.1375
//ACM_AREAV4// 1.1375,1.7812,1.3004,1.3004,1.3004,1.8271,1.4630,1.4630,1.4630,1.8724
//ACM_CAREAW1// 3.9700,3.9700,1.0664,1.4931,4.4109,4.4109,1.0664,1.4721,4.8522,4.8522
//ACM_CAREAW2// 1.0664,1.4507,5.2933,5.2933,1.0664,1.4292,5.7343,5.7343,1.0664,1.4081
//ACM_CAREAW3// 6.1753,6.1753,1.0664,1.3868,6.6166,6.6166,1.0664,1.3653,7.0577,7.0577
//ACM_CAREAW4// 1.0664,1.3437,7.4987,7.4987,1.0664,1.3228,7.9400,7.9400,1.0664,1.3013
//ACM_CAREAH1// 0,0,0.5942,1.1885,0.1981,0.1981,0.6115,1.1763,0.3962,0.3962
//ACM_CAREAH2// 0.6290,1.1639,0.5942,0.5942,0.6463,1.1512,0.7924,0.7924,0.6636,1.1390
//ACM_CAREAH3// 0.9904,0.9904,0.6808,1.1267,1.1885,1.1885,0.6983,1.1144,1.3868,1.3868
//ACM_CAREAH4// 0.7156,1.1016,1.5849,1.5849,0.7329,1.0894,1.7826,1.7826,0.7501,1.0772
//ACM_CAREAV1// 0,0,0.3657,1.0972,0.1624,0.1624,0.5281,1.2013,0.3251,0.3251
//ACM_CAREAV2// 0.6908,1.3049,0.4875,0.4875,0.8532,1.4091,0.6502,0.6502,1.0160,1.5132
//ACM_CAREAV3// 0.8126,0.8126,1.1785,1.6174,0.9753,0.9753,1.3408,1.7215,1.1375,1.1375
//ACM_CAREAV4// 1.5036,1.8255,1.3004,1.3004,1.6662,1.9292,1.4630,1.4630,1.8286,2.0336
wing_area =714.30000
wing_span =71.98000
wing_root_chord =7.55000
wing_dihedral =4.55000
wing_incidence =0.00000
wing_twist =0.00000
oswald_efficiency_factor =0.60000
wing_winglets_flag =1
wing_sweep =5.00000
wing_pos_apex_lon =3.57809
wing_pos_apex_vert =4.28000
htail_area =39.00000
htail_span =17.56000
htail_pos_lon =-19.72000
htail_pos_vert =10.01000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =65.00000
vtail_span =7.44000
vtail_sweep =17.00000
vtail_pos_lon =-17.24000
vtail_pos_vert =2.07000
elevator_area =43.00000
aileron_area =47.00000
rudder_area =43.00000
elevator_up_limit =28.00000
elevator_down_limit =21.00000
aileron_up_limit =25.00000
aileron_down_limit =25.00000
rudder_limit =24.00000
elevator_trim_limit =25.00000
spoiler_limit =60.00000
aileron_to_spoileron_gain =1.00000
spoiler_handle_available =1
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
spoilerons_available =1
spoiler_extension_time=1.00000
auto_spoiler_available=0
positive_g_limit_flaps_up=3.70000
negative_g_limit_flaps_up=-2.96000
positive_g_limit_flaps_down=2.59000
negative_g_limit_flaps_down=-2.22000
load_safety_factor=1.00000


[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17


[jet_engine]
thrust_scalar=1.00000 


[flight_tuning]
cruise_lift_scalar=1.00000 
parasite_drag_scalar=1.00000 
induced_drag_scalar=1.00000 
elevator_effectiveness=1.00000 
aileron_effectiveness=1.00000 
rudder_effectiveness=1.00000 
pitch_stability=1.00000 
roll_stability=1.00000 
yaw_stability=1.00000 
elevator_trim_effectiveness=1.00000 
aileron_trim_effectiveness=1.00000 
rudder_trim_effectiveness=1.00000 
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=0.00000
torque_on_roll=0.00000
gyro_precession_on_roll=0.00000
gyro_precession_on_yaw=0.00000


[TurbineEngineData]
fuel_flow_gain=0.00250 
inlet_area=1.75000 
rated_N2_rpm=15000.00000 
static_thrust=3300.00000 
reverser_available=1 
afterburner_available=0 
afterburner_throttle_threshold=0.00000
ThrustSpecificFuelConsumption=0.00000
AfterBurnThrustSpecificFuelConsumption=0.00000


[Flaps.0]
pan-outboard= 0.75
type= 1
system_type=0
span-outboard= 0.500
extending-time= 5.0
damaging-speed=131.4
blowout-speed=146.0
flaps-position.0=0.00
flaps-position.1=11.25
flaps-position.2=22.50
flaps-position.3=33.75
flaps-position.4=45.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00


[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI


[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1=1 
Com.1=1,1 
Com.2=1,1 
Nav.1=1,1,1 
Nav.2=1,1,0 
Adf.1=1,1 
Transponder.1=1 
Marker.1=1 
Adf.2=0,0


[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0 


[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2 

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0

[brakes]
parking_brake =1
toe_brakes_scale =0.75000
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000

[hydraulic_system]
normal_pressure =3000.00000
electric_pumps  = 0         //no electric pumps
engine_map      = 1,0,0,0   //pump on Eng1

[Views]
eyepoint=10.0, 0, 0.662    //(feet) longitudinal, lateral, vertical distance from reference datum


[exits]
number_of_exits = 2
exit_rate.0 = 0.3                               ;Percent per second
exit_rate.1 = 0.6                               ;Percent per second


[Reference Speeds]
flaps_up_stall_speed=64.99997 
full_flaps_stall_speed=34.99998 
cruise_speed=110.00000 
max_mach                =0.60000
max_indicated_speed     =146.00000


[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1000 
autothrottle_available=0 
pitch_takeoff_ga=8 
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain =0
autothrottle_arming_required=0
default_pitch_mode=0
default_bank_mode=0
use_no_default_bank=1
use_no_default_pitch=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90


[stall_warning]
type=2

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.00000
flap_limit_idle=22.50000
flap_limit_power=16.87500

[AirWrench]
Aircraft_Length=41.50000
Vmax_sl=400.01078
Vmax_ca=149.60127
V_rc=91.94724
Climb_Rate=1141.50000
Climb_Weight=12456.00000
Max_gforce=3.70000
Emergency_hp=0.00000
VSI_Weight=12796.00000
static_margin=0.17900
nose_position_lon=14.50000
ActualIncidence=2.50000
ActualTwist=-1.70000
ActualTailIncidence=2.00000
Aircraft_Type=7
FlowCorrection=1.00000
ReheatCutoff=1.20000
OptimumMach=0.90000
Power_Calibration=1.00000
IdleRPM=0.00000
piston_research=0.00000
JetAltitude=0.00000
turboprop_critical_altitude=4997.49272
target_roll_Vopt=110.01447
target_roll_rate=70.00000
pitch_damping=2.50000
yaw_damping=1.00000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.50000
rudder_scalar=1.00000
dihedral_scalar=0.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=100.00000
Aileron_FF=-100.00000
Roll_Response=30.00000
Adverse_Yaw=0.00000
Control_Response=100.00000
V_Max_Control=201.38633
V_Zero_Control=402.77265
V_Max_RdrControl=201.38633
V_Zero_RdrControl=402.77265
Spin_Stability=100.00000
Roll_Off=2.50000
glide_ratio=12.50966
CritAoA=10.00000
ClAoA_k0=0.10000
ClAoA_k1=0.10000
ClAoA_k2=0.15000
ClAoA_k3=0.15000
Elevator_Propwash=0.00000
Rudder_Propwash=0.00000
afterburner_thrust=3300.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=1
spoiler_cd=0.00000
spoiler_cl=0.00000
spoiler_cm=0.00000
flaps_type=1
flaps_cd_scalar=0.99960
flaps_cm_scalar=0.75000
vfe_enabled=0
gear_cd_scalar=0.00000
gear_cm_scalar=0.00000
critical_mach_number=0.80000
max_mach_cd0=60
direct_edit_drag=0
cylinder_head_temperature=501.00000
exhaust_gas_temperature=600.00000
fuel_pressure=20.00000
oil_pressure=100.00000
oil_temperature=200.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=2.00000
interstage_turbine_temperature=1000.00000
knots_flag=1
cfs1_flag=0
cfs2_flag=0
AI_flag=0
edit_tp_torque=0
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=0
range_est_alt=0.00000
range_est_rpm=0.00000
range_est_mp=29.92000
range_est_fuel=332.00000
contact_light_flags=0
AirWrenchVersion=1.01.64
auto_flaps_enabled=1

[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100