- #Aviones f 22 raptor para armar for free#
- #Aviones f 22 raptor para armar full#
- #Aviones f 22 raptor para armar free#
Wing_pos_apex_vert = 4 Vertical (y) position of wing apex w.r.t reference datum (FEET) 4 is right wing_pos_apex_lon = -1 Longitudinal (z) position of wing apex w.r.t reference datum (FEET) was 5.51747 Wing_sweep = 41 Wing sweep (DEGREES) 45 is right Wing_winglets_flag = 0 Has winglets true/false Oswald_efficiency_factor = 0.9 Wing Oswald efficiency factor e (non dimensional) Wing_twist = 0 Wing twist epsilon (DEGREES) Wing_incidence = 0 Wing incidence (DEGREES) Wing_dihedral = -1.5 Dihedral angle Lambda (DEGREES) Wing_thickness_ratio = 0.008 Local thickness is local_chord(x)*wing_thickness_ratio, x = lateral coord Wing_root_chord = 62 Wing root chord croot (FEET) 60 is right Wing_area = 1450 Wing area S (SQUARE FEET) LeftMain = 10, -3, 1.5, 1343, 0 For each tank: Tank position (z longitudinal, x lateral, y vertical) (FEET), total fuel capacity (GALLONS), unusable fuel capacity (GALLONS)įuel_type = 2 1 = OCTANE 100, 2 = JET_A, 3 = OCTANE 80, 4 = AUTO GAS, 5 = JET Bĭefault_fuel_tank_selector.1 = 1 Default fuel selector used in case of autostart for engine 1, default is ALL.ĭefault_fuel_tank_selector.2 = 1 Default fuel selector used in case of autostart for engine 2, default is ALL.ĭefault_fuel_tank_selector.3 = 1 Default fuel selector used in case of autostart for engine 3, default is ALL.ĭefault_fuel_tank_selector.4 = 1 Default fuel selector used in case of autostart for engine 4, default is ALL.
#Aviones f 22 raptor para armar free#
Max_castering_angle = 3.14159265358979 Defines the maximum angle a free castering wheel can take (in radians). Min_castering_angle = 0.05236 Defines the minimum angle a free castering wheel can take (in radians).
#Aviones f 22 raptor para armar for free#
Max_speed_decreasing_steering_castering = 40 Defines the speed above which the angle of steering stops decreasing for free castering wheels (in feet/second).
#Aviones f 22 raptor para armar full#
Max_speed_full_steering_castering = 20 Defines the speed under which the full angle of steering is available for free castering wheels (in feet/second). Min_available_steering_angle_pct = 0.2 Defines the percentage of steering which will always be available even above max_speed_decreasing_steering (in percent over 100). Max_speed_decreasing_steering = 20 Defines the speed above which the angle of steering stops decreasing (in feet/second). Max_speed_full_steering = 10 Defines the speed under which the full angle of steering is available (in feet/second). Gear_locked_above_speed = -1 Defines the speed at which the landing gear handle becomes locked in the up position. Gear_locked_on_ground = 0 Defines whether or not the landing gear handle is locked to down when the plane is on the ground. Max_number_of_points = 9 Number of contact points Tailwheel_lock = 0 Is tailwheel lock available TRUE/FALSE Gear_system_type = 1 gear system type (betweeen 0 and 4) 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none, 5 = undefined Static_cg_height = 6 feet, altitude of CG when at rest on the ground Static_pitch = 10 degrees, pitch when at rest on the ground (+=Up, -=Dn) Max_number_of_stations = 2 Number of payload stations
Mostly for Concorde).Īctivate_cg_limit_based_on_mach = 0 Activate cg limitation depending on mach value (true if > 0 /false othewise). Reference_datum_position = 0, 0, 0 Position of reference datum relative to FS(0,0,0) (FEET), z, x, yĮmpty_weight_CG_position = 10, 0, 0.2 Position of airplane empty weight CG relative to reference datum (FEET), z, x, yĬG_forward_limit = 0.145 Gravity center forward limit (longitudinal offset) for longitudinal stabilityĬG_aft_limit = 0.28 Gravity center after limit (longitudinal offset z) w.r.t reference datum for longitudinal stability (FEET)Įmpty_weight_pitch_MOI = 69403 Empty pitch moment of inertia, Jxx (SLUG SQ FEET)Įmpty_weight_roll_MOI = 13434 Empty roll moment of inertia, Jzz (SLUG SQ FEET)Įmpty_weight_yaw_MOI = 75997 Empty yaw moment of inertia, Jyy (SLUG SQ FEET)Įmpty_weight_coupled_MOI = 100 Empty transverse moment of inertia, Jyz (SLUG SQ FEET)Īctivate_mach_limit_based_on_cg = 0 Activate mach limitation depending on CG position (true if > 0 /false othewise). Max_gross_weight = 83500 Empty weight, (LBS)Įmpty_weight = 43340 Empty weight, (LBS)
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