//ch47- COPYRIGHT BY V.ZHYHULSKIY - 2004 //=========================================== //=========================================== //=========================================== [fltsim.0] title=CH-47 "Chinook" RAF sim=CH47zh model= panel= sound= texture= checklists= kb_checklists= kb_reference= atc_id=Ch47 atc_airline=RAF atc_flight_number=ZA705 ui_manufacturer=Boeing prop_anim_ratio=-1.12 ui_type=CH47 ui_variation=RAF visual_damage=1 description=CH-47 Boeing RAF atc_heavy=0 [fltsim.1] title=CH-47 "Chinook" UN sim=CH47zh model= panel= sound= texture=UN checklists= kb_checklists= kb_reference= atc_id=Ch47 atc_airline=UN atc_flight_number=ZA705 ui_manufacturer=Boeing prop_anim_ratio=-1.12 ui_type=CH47 ui_variation=UN visual_damage=1 description=CH-47 Boeing UN atc_heavy=0 [General] atc_type=CH47 cHINOOK Boeing Powerplant: Two Textron Lycoming T55-L712 engines Rotor System: Three blades per hub (two hubs) Speed: 225 r/min performance=CH-47 Boeing atc_type=CH47 //=================================================: [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight= 1500.000 =================================== empty_weight_roll_MOI= 9000.000 empty_weight_pitch_MOI= 13000.000 empty_weight_yaw_MOI= 11500.000 empty_weight_coupled_MOI= 1000.000 max_gross_weight= 1900.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 ======================================= [Helicopter] low_realism_stability_scale = 2.5, 1.0, 3.0 ======================================== [fuel] Center1= 0.000, 0.000, 0.000, 110.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 ======================================= [contact_points] point.0= 1.000, 7.333, -10.000, -9.50, 3003.699, 0.000, 0.520, 54.000, 1.121, 2.500, 1.261, 5.000, 5.000, 0.000, 0.000, 0.000 point.1= 1.000, 7.333, 10.000, -9.50, 3003.699, 0.000, 0.520, 54.000, 1.121, 2.500, 1.261, 5.000, 5.000, 0.000, 0.000, 0.000 point.2= 1.000, -21.333, -9.333, -8.70, 3003.699, 1.000, 0.520, 0.000, 1.003, 2.500, 1.416, 8.000, 8.000, 2.000, 0.000, 0.000 point.3= 1.000, -21.333, 9.333, -8.70, 3003.699, 2.000, 0.520, 0.000, 1.003, 2.500, 1.416, 9.000, 9.000, 3.000, 0.000, 0.000 point.4= 2.000, 0.000, -125.000, 50.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 \\point.5= 2.000, 0.000, 125.000, 50.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 \\point.6= 2.000, -50.000, 0.000, -1.667, 1802.219, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 \\point.7= 2.000, 12.500, 0.000, -2.083, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 \\point.8= 4.000, -7.000, -4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 \\point.9= 4.000, -7.000, 4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000 \\point.10= 4.000, 5.350, -4.250, -5.300, 1068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000 \\point.11= 4.000, 5.350, 4.250, -5.300, 1068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000 static_pitch= 1.40 static_cg_height= 8.1 gear_system_type=0 ================================ [GeneralEngineData] engine_type= 3 Engine.0= 10.833, 0.000, 0 Engine.1=-10.833, 0.000, 0 fuel_flow_scalar=1.00000 min_throttle_limit=0.000000 ================================ [fuselage_aerodynamics] drag_force_cf = 0.00 side_drag_force_cf = 1.00 pitch_damp_cf = -1.0 roll_damp_cf = -1.0 yaw_damp_cf = -0.0 yaw_stability_cf = 0.57 =================================== [Reference Speeds] flaps_up_stall_speed=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=0.000000 max_indicated_speed=1000.000000 ===================================== [keyboard_response] elevator=100.000000,180.000000 aileron=200.000000,1000.000000 rudder=200.000000,1000.000000 ================================= [Views] eyepoint=2.609621,-1.755762,-0.0 ========================================== [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=1, -17.95, 0.00, -5.14, fx_beacon , //light.1=4, 8.00, 0.00, 0.90, fx_vclight , //light.2=4, -5.50, 0.00, 0.00, fx_vclight , ================================================= [brakes] toe_brakes_scale=1.300031 parking_brake=1 ===================================== [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 ===================================== [hydraulic_system] normal_pressure=0.000000 ====================================== [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 ============================================= [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second ===================================================================== [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 ===================================================================== [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=1800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [direction_indicators] direction_indicator.0=3,0