[fltsim.0] //Made from C182 from FS2004 //Aircraft designed by John L. Woodward, January 2004 title=MFI-17 Mushshak RAFO-Royal Air Force Oman sim=Saab Safari MFI-15 model= panel=v2 sound= texture=RAFO-Royal Air Force Oman kb_checklists= kb_reference=Saab_ref atc_id= ui_manufacturer=Saab ui_type=Mushshak MFI-15 ui_variation=RAFO Royal Air Force Oman description=FSDS2 model for FS2004 by John L. Woodward, January 2004. atc_airline=MAJAN atc_parking_codes=MF15,M000 atc_parking_types=MIL_COMBAT [General] atc_type=Saab atc_model=Safari editable=1 performance=See Ref page on kneeboard [WEIGHT_AND_BALANCE] max_gross_weight=2646 empty_weight=1424 reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 ;Moments of Inertia empty_weight_pitch_MOI=1400.0 empty_weight_roll_MOI=1137.0 empty_weight_yaw_MOI=2360.0 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=.82 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.75 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw=0 torque_on_roll=0 gyro_precession_on_yaw=0 gyro_precession_on_pitch=0 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-.5, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Fuel flow scalar min_throttle_limit=0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=90 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm=2700 //Max rated RPM max_rated_hp=180 //Max rated HP fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.58 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=8.3 //Propeller moment of inertia beta_max=31.7 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=14.9 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //0 Class //1 Longitudinal Position (feet) //2 Lateral Position (feet) //3 Vertical Position (feet) //4 Impact Damage Threshold (Feet Per Minute) //5 Brake Map (0=None, 1=Left, 2=Right) //6 Wheel Radius (feet) //7 Steer Angle (degrees) //8 Static Compression (feet) (0 if rigid) //9 Max/Static Compression Ratio //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=1, .25, 0.00, -4.40, 1500, 0, 0.65, 20.0, 0.3, 2.5, 0.7, 0.0, 0.0, 0 point.1=1, -5.00, -3.75, -4.35, 2500, 1, 0.75, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 2 point.2=1, -5.00, 3.75, -4.35, 2500, 2, 0.75, 0.0, 0.3, 2.5, 0.7, 0.0, 0.0, 3 max_number_of_points=21 static_pitch=0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=4.35 //feet, altitude of CG when at rest on the ground [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=0.68 //Brake scalar [hydraulic_system] normal_pressure=0.0 //PSI [fuel] //Tanks Position and capacity: //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain=-3.00, 0, 0, 46.0, 0.00 RightMain=-3.00, 0, 0, 46.0, 0.00 //Fuel type: 1=Avgas, 2 = JetA fuel_type=1 number_of_tank_selectors=1 electric_pump=1 [Views] eyepoint= -4.50, -.85, 1.65 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [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 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=100, 180 aileron=200, 1000 rudder=200, 1000 [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=1,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=1,1 //Turn AND Bank [airspeed_indicators] airspeed_indicator.0=1.3, -24.0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0= 3, -3.00, -14.46, 1.87, fx_navred light.1= 3, -3.00, 14.46, 1.87, fx_navgre light.2= 3, -19.85, 0.00, .58, fx_navwhi light.3= 5, .30, 0.00, -3.50, fx_landing [exits] number_of_exits=2 exit_rate.0=0.4 exit_rate.1=0.4 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area=176.0 //Square feet wing_span=36.0 //Feet wing_root_chord=4.9 //Feet wing_dihedral=1.7 //Degrees wing_incidence=1.5 //Degrees wing_twist=-3.0 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=-2.4 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=39.0 //Square feet htail_span=11.7 //Feet htail_pos_lon=-18.3 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=3.2 //Degrees htail_sweep=10.0 //Degrees, horizontal tail leading edge vtail_area=18.0 //Square feet vtail_span=4.8 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-16.2 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.5 //Feet, vertical distance from reference point, positive going up elevator_area=16.6 //Square feet aileron_area=18.3 //Square feet rudder_area=6.7 //Square feet elevator_up_limit=28.0 //Degrees elevator_down_limit=21.0 //Degrees aileron_up_limit=20.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=24.0 //Degrees elevator_trim_limit=19.5 //Degrees spoiler_limit=0.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=54.0 //Knots True (KTAS) full_flaps_stall_speed=49.0 //Knots True (KTAS) cruise_speed=112.0 //Knots True (KTAS) max_indicated_speed=127 //Red line (KIAS) [autopilot] default_bank_mode=0 default_pitch_mode=0 autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.0 [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [stall_warning] type=2
