[fltsim.0]
title=TB1
sim=TB1
model=
panel=
sound=
texture=
checklists=
kb_checklists=
kb_reference=
atc_id=TB1
atc_airline=
atc_flight_number=1123
ui_manufacturer=International Rescue
ui_type=TB1
ui_variation=TB1
description=Thunderbird 1 is the Mach 25 VTOL swing wing rocket/ramjet propelled first response vehicle of the International Rescue fleet. Nuclear reactor for main power, situated aft. Central turbine engine, with bled-off thrust directed through two rings of vectored thrust nozzles, fore and aft. The cross-shaped rear engine cluster contains a mix of ramjets and booster rockets. In horizontal flight, the wings extend from the fuselage to give loitering capability. VTOL rocket emerges from the ventral fuselage for field landings.
First flight October 2nd 1965.
atc_heavy=0
[General]
performance=Length: 115 Feet\nWing span: 87 Feet (Forward Swept)\nWeight: 477,000 lbs Max GWT\nPower: rockets/ramjets\nMax Speed: Mach 23.4 @ 49000 feet\n\nFirst Flight: 23 December 1974 (B-1A)\nComputer simulation by: Ken Bertschy. Flight performance data by Harold Sanders who has no idea that I lifted the data from his excellent B1b Lancer simulation\n
atc_type=
atc_model=
Category=airplane
[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=7500.000
empty_weight_roll_MOI=80000.000
empty_weight_pitch_MOI=145000.000
empty_weight_yaw_MOI=100000.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=18890.000
CG_forward_limit=0.000
CG_aft_limit=1.000
[flight_tuning]
critcal_altitude=40000
cruise_lift_scalar=1.0
parasite_drag_scalar=3
induced_drag_scalar=2
elevator_effectiveness=6
aileron_effectiveness=1
rudder_effectiveness=2.5
pitch_stability=25
roll_stability=4
yaw_stability=1
elevator_trim_effectiveness=1.5
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[brakes]
toe_brakes_scale=4.7000061
parking_brake=1
differential_braking_scale = 1.0
[fuel]
LeftMain=0.000, 0.000, 0.000, 800.000, 0.000
LeftAux=0.000, -18.250, 0.000, 50.000, 0.000
RightMain=0.000, 0.000, 0.000, 800.000, 0.000
RightAux=0.000, 18.250, 0.000, 50.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=1001.000
wing_span=45.833
wing_root_chord=21.833
wing_dihedral=3.999
wing_incidence=-0.494
wing_twist=-1.000
oswald_efficiency_factor=3.501
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=0.000
wing_pos_apex_vert=0.000
htail_area=200.000
htail_span=21.583
htail_pos_lon=-20.833
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=350.000
vtail_span=21.331
vtail_sweep=0.000
vtail_pos_lon=-12.500
vtail_pos_vert=5.833
elevator_area=50.000
aileron_area=40.040
rudder_area=59.500
elevator_up_limit=27.502
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=23.491
elevator_trim_limit=19.481
spoiler_limit=59.989
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000
auto_spoiler_available=1
spoiler_extension_time=5.000000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=3.000000
negative_g_limit_flaps_up=-3.000000
negative_g_limit_flaps_down=-2.000000
[contact_points]
point.0=1.000000,66.000000,0.000000,-10.666667,1574.803150,0.000000,3.187522,72.480000,0.544105,2.500000,0.480601,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,-7.333333,-6.583333,-10.666667,1574.803150,1.000000,3.187522,0.000000,0.544112,2.500000,0.480603,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,-7.333333,6.583333,-10.666667,1574.803150,2.000000,3.187522,0.000000,0.544112,2.500000,0.480603,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,-10.500000,-68.500000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-10.500000,68.500000,-2.000000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-57.833333,0.000000,-0.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,59.000000,0.000000,-0.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=10.669300
gear_system_type=0
[Lights]
light.0 = 5, 5, 1, 1.5, fx_shockwave_landing_light_narrow_down_45,
light.1 = 5, 5, 2, 1.5, fx_shockwave_landing_light_narrow_down_45,
light.2 = 1,-50, 2, 29, fx_beacon ,
light.3 = 7, -55.5, 2, 1, fx_cylonflame,
light.4 = 7, -55.5, 2, 19, fx_cylonflame,
light.5 = 7, -55.5, 2, 10, fx_cylonflame,
light.6 = 7, -55.5, 17.8, 10.1, fx_Bob_Burn_blue,
light.7 = 7, -55.5, 11.4, 10.1, fx_Bob_Burn_blue,
light.8 = 7, -55.5, -12.9, 10.1, fx_Bob_Burn_blue,
light.9 = 7, -55.5, -7.1, 10.1, fx_Bob_Burn_blue,
light.10 = 10, -51.5, -12, 5, fx_Bob_FlameDown, //Flame Downward
light.11 = 10, -51.5, 18, 5, fx_Bob_FlameDown, //Flame Downward
light.12 = 10, -45.5, -12, 5, fx_Bob_FlameDown, //Flame Downward
light.13 = 10, -45.5, 18, 5, fx_Bob_FlameDown, //Flame Downward
light.14 = 9, -55.5, 2, 1, fx_RCB_SmokeHor, //Smoke Backward
light.15 = 9, -55.5, 2, 19, fx_RCB_SmokeHor, //Smoke Backward
light.16 = 9, -55.5, 2, 10, fx_RCB_SmokeHor, //Smoke Backward
light.17 = 8, -51.5, -12, 5, fx_RCB_SmokeVert, //Smoke Downward
light.18 = 8, -51.5, 18, 5, fx_RCB_SmokeVert, //Smoke Downward
light.19 = 8, -45.5, -12, 5, fx_RCB_SmokeVert, //Smoke Downward
light.20 = 8, -45.5, 18, 5, fx_RCB_SmokeVert, //Smoke Downward
[GeneralEngineData]
engine_type=1
Engine.0=0.000, 0.001, 0.000
fuel_flow_scalar=0.010
min_throttle_limit=-0.250000
[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
[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=31.861
rated_N2_rpm=29920.000
static_thrust=90000.600
afterburner_available=1
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=10.000
full_flaps_stall_speed=8.000
cruise_speed=600.892
max_indicated_speed=2000.093750
max_mach=1.7
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[Views]
eyepoint=8.650652,-0.025632,3.075787
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=5.000000
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_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
[SMOKESYSTEM]
smoke.0 = 0,4,10, fx_RCB_machenvlop, //0,70,0
[Flaps.0]
type=1
span-outboard=0.500
extending-time=3.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=80.000, 00.000
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[pitot_static]
pitot_heat=1.000000
[hydraulic_system]
normal_pressure=0.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[deice_system]
structural_deice_type=0
