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Problem with Tom Ruth DC-10 Series


kolokoysz8x8

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Hi guys, I'm pretty new here in using the forums so I apologize in advance if I did anything wrong while I post this message.

 

Recently I've downloaded Tom Ruth and Eric Cantu's DC-10 Series. I want to ask if anyone among you guys have cracked the problem with the model's "Push Back" contact_points in the aircraft.cfg file of the model.

 

I've been searching the answer for several hours now with no luck at all, and I was hoping if anyone among you can give me the correct contact_points for the aircraft. Specifically we are talking about the -30 version of the DC-10.

 

Thank you in advance

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I fly the T. Ruth DC-10. What problem do you have with the contact points of, I'm guessing, the nose wheel?? I'll list my contact points.

 

[contact_points]

 

;/0 Class

;/1 Longitudinal Position (feet)

;/2 Lateral Position (feet)

;/3 Vertical Position (feet)

;/4 Impact Damage Threshold (Feet Per Minute)

;/5 Brake Map (0=None, 1=Left, 2=Right)

;/6 Wheel Radius (feet)

;/7 Steer Angle (degrees)

;/8 Static Compression (feet) (0 if rigid)

;/9 Max/Static Compression Ratio

;/10 Damping Ratio (0=Undamped, 1=Critically Damped)

;/11 Extension Time (seconds)

;/12 Retraction Time (seconds)

;/13 Sound Type

;/14 Airspeed limit for retraction (KIAS)

;/15 Airspeed that gear gets damage at (KIAS)

; 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15

;----------------------------------------------------------------------------------------------------

point.0 = 1, 67.155, 0, -12.38, 1200, 0, 1.68, 90, 0.590, 3.361, 0.72, 8, 9, 0, 180, 250

point.1 = 1, -12.3114, -18.2, -12.38, 1500, 1, 2.51, 0, 0.590, 2.849, 0.74, 9.9, 10.9, 2, 180, 250

point.2 = 1, -12.3114, 18.2, -12.38, 1500, 2, 2.51, 0, 0.590, 2.849, 0.74, 9.1, 10.1, 3, 180, 250

point.3 = 2, -34.00, -86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0

point.4 = 2, -34.00, 86.00, 8.40, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0

point.5 = 2, 61.8791, 0, -3.1502, 787, 0, 0.0, 0, 0, 0, 0, 0, 0, 9, 0, 0

point.6 = 2, -93.50, 0.00, 25.00, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0

point.7 = 2, -85.50, 0.00, 11.50, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0

point.8 = 2, -46.50, 0.00, -1.65, 787, 0, 0.0, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0

Still thinking about a new flightsim only computer!  ✈️

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