[fltsim.0] title=Sud-Ouest Djinn sim=djinn model= panel= sound= texture= kb_checklists= kb_reference= prop_anim_ratio=-1.2 atc_id_color=0xc6eff7ff atc_id=N834JR atc_model= ui_manufacturer=Sud Ouest ui_type="Djinn" ui_variation="Swift Copters & Rotomobil colors" description=The Djinn was the world's first production helicopter to make use of the 'cold jet' principle of propulsion. The term 'cold jet' indicates simply that compressed air from the gas turbine engine is ducted through channels inside the rotor blades and expelled through nozzles at their tips The first of which made its maiden flight on 2 January 1953. In the Djinn, torque reaction was offset by a turbine jet deflector mounted at the tail, which could be rotated to act as a rudder as well [General] atc_type=JetRanger performance="Cruise Speed \t\n70 kts 81 mph 130 km\/h\n\nEngine\nTurbomeca Palouste IV 240 shp\n\nMaximum Range\n102 nm \t 190 km\n\nService Ceiling\n13,200 ft 4000 m\n\nHovering Ceiling\n \n\nFuel Capacity\n U.S. gal L\n\nEmpty Weight\n790 lb 360 kg\n\nMaximum Gross Weight\n1670 lb 760 kg\n\nMaximum Gross Weight (External Loading)\n lb kg\n\nLength\t\n ft\t 5.30 m\n\nRotor Span\n ft\t 10.97 m\n\nHeight\n ft\t 2.60 m\n\nSeating \t\n2 \n\nUseful Load\t\n lb\t kg\n" editable=0 [WEIGHT_AND_BALANCE] max_gross_weight=3200 // (pounds) empty_weight=1760 // (pounds) reference_datum_position=0.0, 0.0, 0.0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0.0, 0.0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0="170, 0.0, -1.17, 0.0, Co-Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1="170, 0.0, 1.17, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2="0, 0.0, -1.42, 0.0, Passenger 1" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3="0, 0.0, 0.00, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4="0, 0.0, 1.42, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5="0, 0.0, 0.00, 0.0, Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=6000 empty_weight_roll_MOI=4000 empty_weight_yaw_MOI=10000 empty_weight_coupled_MOI=0 [turboprop_engine] power_scalar=1.0 [propeller] thrust_scalar=1.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Helicopter] low_realism_stability_scale=1.0, 1.0, 1.0 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings [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 <0=none,1=wheel, 2=scrape, 3=skid> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) [contact_points] point.0=3, 4.83, 3.33, -4.50, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 7.0, 0.0, 0.0 point.1=3, -3.50, -3.33, -4.58, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 7.0, 0.0, 0.0 point.2=3, -3.50, 3.33, -4.58, 1574.8, 0, 0.5187, 0.0, 0.396299, 2.5, 0.728164, 0.0, 0.0, 7.0, 0.0, 0.0 point.3=3, 4.83, -3.33, -4.50, 1574.8, 0, 0.5187, 0.0, 0.286975, 2.5, 0.605067, 0.0, 0.0, 7.0, 0.0, 0.0 point.4=2, 0.00, -16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 5.0, 0.0, 0.0 point.5=2, 0.00, 16.67, 9.00, 0.0, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 6.0, 0.0, 0.0 point.6=2, -20.50, 0.00, 1.67, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 9.0, 0.0, 0.0 point.7=2, 0.00, 9.08, 2.58, 787.4, 0, 0.0000, 0.0, 0.000000, 0.0, 0.000000, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch=0.198 static_cg_height=4.294 [brakes] parking_brake=0 //Parking brake available toe_brakes_scale=0.0 //Brake scalar [hydraulic_system] normal_pressure=0.0 //PSI [Views] eyepoint=1.8, 1.5, 2.2 [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. //NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque 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=3,0 [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=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=1, -2.00, 0.00, -3.20, fx_beacon , light.1=2, -10.60, 0.00, -2.70, fx_strobe , light.2=4, 2.00, 0.00, 1.50, fx_vclight , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks [fuel] Center1=0.0, 0.0, 0.0, 91.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=8.3, 0.0, 0.4 //(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 [Reference Speeds] flaps_up_stall_speed=0.0 //Knots True (KTAS) full_flaps_stall_speed=0.0 //Knots True (KTAS) cruise_speed=115.0 //Knots True (KTAS) max_indicated_speed=130 //Red line (KIAS) [autopilot] autopilot_available=0 flight_director_available=0 [yaw_string] yaw_string_available=1
