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Alt 11.08.2005, 15:22   #14
jorg202
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Registriert seit: 27.12.2003
Beiträge: 637


Standard

hatte übersehen, dass der flieger unbeladen "ausgeliefert" wird!
wenn man den vogel belädt, ist man fast wieder versucht, den thrust_scalar=1.250 auf 1.400 einzustellen!

[WEIGHT_AND_BALANCE]
max_gross_weight= 502000.000
empty_weight= 244000.000
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 = "180.0, 86.0, -2.0, 0.0, Pilot" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.1 = "180.0, 86.0, 2.0, 0.0, Kopilot" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.2 = "1000.0, 0.0, 0.0, 0.0, Besatzung" //Weight (lbs),

longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "1000.0, 52.0, 0.0, 0.0, Erste Klasse" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.4 = "2000.0, 11.0, 0.0, 0.0, Businessklasse" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.5 = "6000.0, -30.0, 0.0, 0.0, Sitze vorn" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.6 = "5000.0, -72.5, 0.0, 0.0, Sitze hinten" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.7 = "60000.0, 47.0, 0.0, -6.0, Fracht vorne" //Weight (lbs), longitudinal,

lateral, vertical positions from datum (feet)
station_load.8 = "50000.0, -67.0, 0.0, -6.0, Fracht hinten" //Weight (lbs),

longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI= 24000000.000
empty_weight_roll_MOI= 5500000.000
empty_weight_yaw_MOI= 16300000.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
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