ROC-v2.0
AEROLAB
Project: Frostfire 2

Normal_Coefficient_Unit: Per_Radian
Length_Unit_is: mm
* 0.00000000000000E+0000# 1.00000000000000E+0000
AUTOMATIC:  4.40609155064132E+0003  Reference Length:  1.00000000000000E+0000

Nose_Type: Power 1/2
Length:  1.00000000000000E+0002  Diameter:  7.49000000000000E+0001  Form: 0.000000
Surface_Roughness:  1.05338697514777E-0004
Length_From_Nose_Tip_To_Exit_Plane:  1.86300000000000E+0003
Nozzle_Diameter:  0.00000000000000E+0000
Number_of_Conical_Transitions_in_Rocket: 0
Cylindrical_Body_Tube_Part
Diameter:  7.49000000000000E+0001  Length:  1.76300000000000E+0003  Distance_from_Nose_Tip:  1.00000000000000E+0002
Forward_Fin_Parameters
Number_of_Fins: 3
Fin_Location:  1.63300000000000E+0003
Fin_Root_Chord:  1.80000000000000E+0002
Fin_Tip_Chord:  8.00000000000000E+0001
Fin_Transition:  6.00000000000000E+0001
Fin_Semispan:  6.80000000000000E+0001
Fin_Root_Leading_Wedge:  2.00000000000000E+0000
Fin_Root_Trailing_Wedge:  1.00000000000000E+0001
Fin_Root_Thickness:  2.00000000000000E+0000
Fin_Tip_Leading_Wedge:  2.00000000000000E+0000
Fin_Tip_Trailing_Wedge:  1.00000000000000E+0001
Fin_Tip_Thickness:  2.00000000000000E+0000
Fin_Body_Diameter:  7.49000000000000E+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:  2.00000000000000E+0000
Lug_Length:  1.00000000000000E+0001

END