ROC-v2.0
AEROLAB
Project: Frostfire 3

Normal_Coefficient_Unit: Per_Radian
Length_Unit_is: mm
* 0.00000000000000E+0000# 1.30000000000000E+0000
AUTOMATIC:  7.51220776919045E+0003  Reference Length:  1.00000000000000E+0000

Nose_Type: Power 3/4
Length:  2.95000000000000E+0002  Diameter:  9.78000000000000E+0001  Form: 0.000000
Surface_Roughness:  5.06000000000000E-0006
Length_From_Nose_Tip_To_Exit_Plane:  2.04600000000000E+0003
Nozzle_Diameter:  5.00000000000000E+0001
Number_of_Conical_Transitions_in_Rocket: 0
Cylindrical_Body_Tube_Part
Diameter:  9.78000000000000E+0001  Length:  1.75100000000000E+0003  Distance_from_Nose_Tip:  2.95000000000000E+0002
Forward_Fin_Parameters
Number_of_Fins: 6
Fin_Location:  1.88100000000000E+0003
Fin_Root_Chord:  1.65000000000000E+0002
Fin_Tip_Chord:  8.25000000000000E+0001
Fin_Transition:  4.05000000000000E+0001
Fin_Semispan:  8.28000000000000E+0001
Fin_Root_Leading_Wedge:  8.25000000000000E+0001
Fin_Root_Trailing_Wedge:  8.25000000000000E+0001
Fin_Root_Thickness:  5.00000000000000E+0000
Fin_Tip_Leading_Wedge:  4.12500000000000E+0001
Fin_Tip_Trailing_Wedge:  4.12500000000000E+0001
Fin_Tip_Thickness:  3.00000000000000E+0000
Fin_Body_Diameter:  9.78000000000000E+0001
Fin_Canting_Angle:  0.00000000000000E+0000

Aft_Fin_Parameters
Number_of_Fins: 0

Launch_Lugs
Number_of_Lugs: 2
Lug_Height:  5.00000000000000E+0000
Lug_Width:  1.00000000000000E+0001
Lug_Thickness:  1.00000000000000E+0000
Lug_Length:  1.00000000000000E+0001

PARTLIST
1
Complete rocket
User Object
User Mater
 1.44600000000000E+0000
 8.10500000000000E+0000
 1.00000000000000E+0003
1
1
0
 0.00000000000000E+0000
 8.10500000000000E+0000
 8.10500000000000E+0000
 0.00000000000000E+0000
 0.00000000000000E+0000
 0.00000000000000E+0000
END