//mod.stand: märz 2003
[fltsim.0]
title=S-72_2002
sim=S-72 HR mod
model=
panel=
sound=
texture=
kb_checklists=S72_check
kb_reference=S72_CHECK
DESCRIPTION=The RSRA ( Rotor Systems Research Aircraft ) was developed by Sikorsky for NASA and the Army. Configured with rotor, wings and auxiliary jets, the RSRA allows testing of new rotor concepts at speeds up to 300 knots. It can fly like a helicopter with a wing and jets, or as a fixed-wing aircraft without a rotor. The RSRA was a unique pure research aircraft developed to fill the void between design analysis, wind tunnel testing, and flight results of rotor aircraft. The joint NASA/Army project began in December of 1970, first flight on October 12, 1976 with the first of two aircraft arriving from Sikorsky to NASA on February 11, 1979. The aircraft was designed to investigate the concepts involved with stopping the main rotor in flight, with the large blades then providing aerodynamic lift assistance to the stubby conventional wings extending from the lower fuselage. This concept gave the aircraft the vertical flight stability of a helicopter, and the horizontal cruise capability of a conventional aircraft.
atc_id=545
atc_flight_number=545
UI_MANUFACTURER=Sikorsky
ui_type=S-72
ui_variation=545 -- new FS2K2
[General]
PERFORMANCE= ***CLASSIFIED***\nTo swich to Helicopter mode, lower flaps, idle throttle, then extract spoilers, wait 20 seconds. Now rtetract flaps. Use rudder and elevator to control, and throttle as collective lever. Use alierons to fine-tune your flight.
editable=0
ATC_TYPE=SIKORSKY
ATC_MODEL=S72
performance=\n\n\n
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing (long,lat,vert);
light.0=3, 14.17, 49.20, -2.48, fx_navgreh ,//right wing;
light.1=3, 14.17, -49.20, -2.48, fx_navredh ,//left wing;
light.2=4, 53.80, 0.00, 5.80, fx_vclight_h ,//cockpit;
[weight_and_balance]
// ACM V2.0
max_gross_weight = 31837.1
empty_weight = 15000
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 5, 0, 0
empty_weight_pitch_MOI = 1650000
empty_weight_roll_MOI = 600000
empty_weight_yaw_MOI = 1300000
empty_weight_coupled_MOI = 2000
max_number_of_stations = 1
station_load.0 = 5000, 5, 0, 0
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 1
fuel_flow_scalar = 1.0
engine.0 = 14.72, 0, 13,
engine.1 = 25.5, 15.5, 2.5,
engine.2 = 25.5, -15.5, 2.5,
[smokesystem]
smoke.0 = 0, 4.5, -4, fx_S72_smoke1
smoke.1 = 0, 4.5, 4, fx_S72_smoke1
smoke.2 = 0, -14.5, 0, fx_S72_smoke2
smoke.3 = 0, 6, -16, fx_S72_smoke3
smoke.4 = 0, 6, 16, fx_S72_smoke3
smoke.5 = 0, 6, -16, fx_S72_smoke4
smoke.6 = 0, 6, 16, fx_S72_smoke4
smoke.7 = 0, 2.83, 50.2, fx_S72_tip_vort
smoke.8 = 0, 2.83, -50.2, fx_S72_tip_vort
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 1
Center1 = 0, 0, 0, 2000, 0
[contact_points]
static_pitch = 4.340723
static_cg_height = 9.413105
max_number_of_points = 7
point.0 = 1, -65.731, 0, -5.7922, 2574.80315, 0, 0.528014, 45, 1.476734, 2.5, 0.928518, 8, 8, 1, 0, 0
point.1 = 1, 31, -11.6666, -13.5, 2574.80315, 1, 1.528014, 0, 1.961321, 2.5, 0.919541, 8, 8, 2, 0, 0
point.2 = 1, 31, 11.666667, -13.5, 2574.80315, 2, 1.528014, 0, 1.961321, 2.5, 0.919541, 8, 8, 3, 0, 0
point.3 = 2, 7.583333,-51.166667,-2.333333, 1500,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4 = 2, 7.583333, 51.166667,-2.333333, 1500,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5 = 2, -84.6849, 0, 20.6955, 787.40157, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 70.333333, 0.000000, 0.000000, 787.40157,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[airplane_geometry]
//ACM_AREAW1// 2.1175,2.1175,0.1624,7.3182,3.8076,3.8076,0.4465,7.2361,5.2533,5.2533
//ACM_AREAW2// 0.6485,7.0724,6.8621,6.8621,1.0951,7.1531,8.1449,8.1449,1.3789,7.0707
//ACM_AREAW3// 10.0794,10.0794,1.7438,6.9071,11.6878,11.6878,1.9462,6.8248,13.1337,13.1337
//ACM_AREAW4// 2.2297,6.5795,14.2538,14.2538,2.4319,6.4159,15.4553,15.4553,3.3673,5.6820
//ACM_AREAH1// 0,0,0,1.8301,0.7501,0.7501,0,1.7711,1.5246,1.5246
//ACM_AREAH2// 0,1.7841,2.2506,2.2506,0,1.7733,3.0734,3.0734,0,1.7863
//ACM_AREAH3// 4.0163,4.0163,0,1.7755,4.8147,4.8147,0,1.7890,5.6374,5.6374
//ACM_AREAH4// 0,1.7539,6.5802,6.5802,0,1.7668,7.6272,7.6272,0,1.7797
//ACM_AREAV1// -0.0511,-0.0511,0,5.1398,0.5938,0.5938,0.6654,5.6050,1.1876,1.1876
//ACM_AREAV2// 1.1770,6.0700,1.9349,1.9349,1.9960,6.5352,2.8872,2.8872,3.3271,7.3074
//ACM_AREAV3// 3.7881,3.7881,4.2484,7.8748,4.6890,4.6890,5.3744,8.5445,5.5900,5.5900
//ACM_AREAV4// 6.5005,9.2145,6.4397,6.4397,7.3708,9.7306,7.5967,7.5967,8.7529,10.5031
//ACM_CAREAW1// 7.6103,7.6103,5.5324,7.0043,8.4146,8.4146,5.5998,6.9408,9.2187,9.2187
//ACM_CAREAW2// 5.6304,6.8400,9.9862,9.9862,5.6606,6.7765,10.6420,10.6420,5.6911,6.7501
//ACM_CAREAW3// 11.4834,11.4834,5.6472,6.7234,12.2135,12.2135,5.6777,6.6599,12.9062,12.9062
//ACM_CAREAW4// 5.7452,6.5591,13.6736,13.6736,5.7385,6.4583,14.3294,14.3294,5.8060,6.5061
//ACM_CAREAH1// 0.3411,0.3411,1.1533,1.8157,0.9818,0.9818,1.1533,1.8055,1.5814,1.5814
//ACM_CAREAH2// 1.1541,1.7798,2.3036,2.3036,1.1412,1.8229,3.0269,3.0269,1.1555,1.7583
//ACM_CAREAH3// 3.9251,3.9251,1.1425,1.8018,4.9464,4.9464,1.1563,1.7640,6.0068,6.0068
//ACM_CAREAH4// 1.1433,1.7941,6.9477,6.9477,1.1447,1.7841,7.6026,7.6026,1.1488,1.7739
//ACM_CAREAV1// -0.2630,-0.2630,-20.0342,-16.2425,0.7379,0.7379,-19.8805,-16.5102,1.3621,1.3621
//ACM_CAREAV2// -19.8805,-16.5335,1.9349,1.9349,-19.8805,-16.6081,2.3450,2.3450,-19.7782,-16.7642
//ACM_CAREAV3// 2.7760,2.7760,-19.8295,-16.8595,3.6561,3.6561,-19.8295,-17.3320,4.4337,4.4337
//ACM_CAREAV4// -19.8292,-17.5694,5.1810,5.1810,-19.7782,-17.5531,5.6213,5.6213,-19.7782,-17.6487
wing_area = 1963.000000
wing_span = 101.94
wing_root_chord = 23.20
wing_dihedral = 2.5
wing_incidence = 0.000000
wing_twist = -0.999756
oswald_efficiency_factor = 1.5
wing_winglets_flag = 0
wing_sweep = 10
wing_pos_apex_lon = 23.51
wing_pos_apex_vert = -5.07
htail_area = 291.000000
htail_span = 50.52
htail_pos_lon = -57.13
htail_pos_vert = 1.58
htail_incidence = 0.000000
htail_sweep = 0
vtail_area = 295.000000
vtail_span = 24.93
vtail_sweep = 50
vtail_pos_lon = -53.40
vtail_pos_vert = 3.25
elevator_area = 99.900000
aileron_area = 152.000000
rudder_area = 183.200000
elevator_up_limit = 21.719698
elevator_down_limit = 20.281951
aileron_up_limit = 23.697534
aileron_down_limit = 23.124577
rudder_limit = 22.689129
elevator_trim_limit = 19.996227
spoiler_limit = 59.988681
aileron_to_spoileron_gain = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons = 0.000000
spoilerons_available = 0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=19.600000
rated_N2_rpm=29920.000000
static_thrust=10500.000000
afterburner_available=0
reverser_available=1
[jet_engine]
thrust_scalar=1.0
[Reference Speeds]
flaps_up_stall_speed=130.000000
full_flaps_stall_speed=130.000000
cruise_speed=280.00
[Views]
eyepoint=14.994464,-2.063341,-4.908444
[autopilot]
autopilot_available=1
flight_director_available=0
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
[direction_indicators]
direction_indicator.0=3,0
[Flaps.0]
type=1
span-outboard=1.5
extending-time=8.0
system_type=0
flaps-position.0=0
flaps-position.1=8
flaps-position.2=17
flaps-position.3=25
