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Data CatalogΒΆ

Name

Value

File

a

stub_length

fuselage/rear_hook/rear_hook_data.scad

tip_dihedral

wing/wing_data.scad

b

ms_height - wire_diameter

fuselage/rear_hook/rear_hook_data.scad

(max_projected_wing_span - center_span)/2

wing/wing_data.scad

bend_radius

1.5*wire_diameter

fuselage/rear_hook/rear_hook_data.scad

c

2.5

prop/prop_data.scad

hook_side

fuselage/rear_hook/rear_hook_data.scad

center_span

6

stab/stab_data.scad

12

wing/wing_data.scad

density

501.12

fuselage/rear_hook/rear_hook_data.scad

168.77

fuselage/thrust_bearing/thrust_bearing_data.scad

6

fuselage/tail_boom/tail_boom_data.scad

f

2

prop/prop_data.scad

fin_chord

4

fuselage/fin/fin_data.scad

fin_color

WOOD_Balsa

fuselage/fin/fin_data.scad

fin_le_length

fin_span - fin_radius - spar_size

fuselage/fin/fin_data.scad

fin_radius

1.5

fuselage/fin/fin_data.scad

fin_span

2

fuselage/fin/fin_data.scad

fin_te_length

fin_span -2*spar_size

fuselage/fin/fin_data.scad

fp_offset

wing_offset - post_diameter/2 - tube_thickness

fuselage/fuselage_data.scad

fuse_offset

thb_length - thb_top_length - 3 * tube_thickness

fuselage/fuselage_data.scad

hook_offset

thb_height

fuselage/rear_hook/rear_hook_data.scad

hook_side

(hook_offset - 2*bend_radius*ka)/ka

fuselage/rear_hook/rear_hook_data.scad

ka

sin(45)

fuselage/rear_hook/rear_hook_data.scad

motor_stick_rear_height

0.1875

fuselage/motor_stick/motor_stick_data.scad

motor_stick_thickness

1/8

math_magik_lpp_data.scad

ms_height

motor_stick_rear_height

fuselage/rear_hook/rear_hook_data.scad

ms_length

10

fuselage/motor_stick/motor_stick_data.scad

ms_points

fuselage/motor_stick/motor_stick_data.scad

ms_thickness

1/8

fuselage/motor_stick/motor_stick_data.scad

num_center_ribs

3

stab/stab_data.scad

5

wing/wing_data.scad

p1

[-bend_radius,0,b]

fuselage/rear_hook/rear_hook_data.scad

p2

[-bend_radius,0,0]

fuselage/rear_hook/rear_hook_data.scad

p3

p2 + [bend_radius*ka,0,-bend_radius*ka]

fuselage/rear_hook/rear_hook_data.scad

p4

p3 + [-hook_side*ka, 0,-hook_side*ka] + [bend_radius*ka,0,-bend_radius*ka]

fuselage/rear_hook/rear_hook_data.scad

p5

p4 + [-bend_radius*ka,0,-bend_radius*ka]

fuselage/rear_hook/rear_hook_data.scad

post_size

1/16

math_magik_lpp_data.scad

prop_blade_color

WOOD_Balsa

prop/prop_data.scad

prop_blade_offset

0.5

prop/prop_data.scad

prop_blade_thickness

1/64

prop/prop_data.scad

prop_form_angle

14

prop/prop_data.scad

prop_form_height

prop_radius + 2

prop/prop_data.scad

prop_form_radius

2.5

prop/prop_data.scad

prop_forward_x

-1.3287

prop/prop_data.scad

prop_max_chord

1.85

prop/prop_data.scad

prop_pitch_angle

40

prop/prop_data.scad

prop_radius

max_prop_diameter/2

prop/prop_data.scad

prop_spar_color

WOOD_Balsa

prop/prop_data.scad

prop_spar_inner_radius

1/32

prop/prop_data.scad

prop_spar_length

4

prop/prop_data.scad

prop_spar_outer_radius

1/64

prop/prop_data.scad

prop_x_offset

-1/4 - 1/32

math_magik_lpp_data.scad

1/16

fuselage/fuselage_data.scad

prop_x_width

1.3287

math_magik_lpp_data.scad

prop_z_offset

-3/16

math_magik_lpp_data.scad

thb_height

fuselage/fuselage_data.scad

r

wire_diameter/2

fuselage/rear_hook/rear_hook_data.scad

rear_hook_color

METAL_Steel

fuselage/rear_hook/rear_hook_data.scad

rib_camber

2

stab/stab_data.scad

4

wing/wing_data.scad

rib_chord

max_stab_chord - 2 * spar_size

stab/stab_data.scad

max_wing_chord - 2 * spar_size

wing/wing_data.scad

rp_offset

wing_offset + max_wing_chord + post_diameter/2 + tube_thickness

fuselage/fuselage_data.scad

rubber_motor_length

10

rubber_motor/rubber_motor_data.scad

rubber_motor_radius

1/8

rubber_motor/rubber_motor_data.scad

s

prop_radius - 1

prop/prop_data.scad

s1

1

prop/prop_data.scad

s2

s - s1

prop/prop_data.scad

s3

1

prop/prop_data.scad

s4

1

prop/prop_data.scad

sfp_offset

srp_offset - max_stab_chord - post_diameter - tube_thickness-1/64

fuselage/fuselage_data.scad

spar_size

1/16

stab/stab_data.scad

1/32

fuselage/fin/fin_data.scad

1/16

wing/wing_data.scad

srp_offset

tail_boom_rear_x - post_diameter - tube_thickness-1/16

fuselage/fuselage_data.scad

stab_center_span

6

math_magik_lpp_data.scad

stab_elevation

0.5

math_magik_lpp_data.scad

stab_post_color

WOOD_Balsa

fuselage/stab_post/stab_post_data.scad

stab_post_height

0.5 + tube_height

fuselage/stab_post/stab_post_data.scad

stab_rib_camber

2

math_magik_lpp_data.scad

stab_tip_radius

1.5

math_magik_lpp_data.scad

stab_x_offset

max_overall_length - prop_x_width - max_stab_chord

math_magik_lpp_data.scad

stub_length

1/8

fuselage/rear_hook/rear_hook_data.scad

tail_boom_angle

atan2(tb_front_height - tb_rear_height,tail_boom_length)

fuselage/fuselage_data.scad

atan2(tb_front_height - tb_rear_height,tail_boom_length)

fuselage/tail_boom/tail_boom_data.scad

tail_boom_length

max_overall_length -ms_length + prop_forward_x + tail_boom_overlap

fuselage/fuselage_data.scad

tail_boom_overlap

1/8

fuselage/fuselage_data.scad

tail_boom_rear_x

max_overall_length + prop_x_offset

fuselage/fuselage_data.scad

tb_color

WOOD_Balsa

fuselage/fuselage_data.scad

WOOD_Balsa

fuselage/tail_boom/tail_boom_data.scad

tb_front_height

3/16

fuselage/fuselage_data.scad

3/16

fuselage/tail_boom/tail_boom_data.scad

tb_rear_height

1/16

fuselage/fuselage_data.scad

1/16

fuselage/tail_boom/tail_boom_data.scad

tb_thickness

3/32

fuselage/fuselage_data.scad

3/32

fuselage/tail_boom/tail_boom_data.scad

thb_front_height

thb_height/3

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_height

3/16

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_length

1/2

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_thickness

1/32

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_top_length

3/16

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_width

1/16

fuselage/thrust_bearing/thrust_bearing_data.scad

thb_wire_size

0.025

fuselage/thrust_bearing/thrust_bearing_data.scad

thrust_bearing_color

METAL_Aluminium

fuselage/thrust_bearing/thrust_bearing_data.scad

thrust_bearing_x_offset

-1/4

math_magik_lpp_data.scad

tip_dihedral

1.75

wing/wing_data.scad

tip_dihedral_angle

atan2(a,b)

wing/wing_data.scad

tip_le_span

tip_span - tip_radius

stab/stab_data.scad

tip_span - tip_radius

wing/wing_data.scad

tip_radius

1.5

stab/stab_data.scad

2

wing/wing_data.scad

tip_rib_chord

max_stab_chord - tip_radius - spar_size

stab/stab_data.scad

max_wing_chord - tip_radius - spar_size

wing/wing_data.scad

tip_span

(max_stab_span - center_span)/2

stab/stab_data.scad

sqrt(a*a + b*b)

wing/wing_data.scad

wing_center_span

12

math_magik_lpp_data.scad

wing_elevation

3

math_magik_lpp_data.scad

3

fuselage/fuselage_data.scad

wing_offset

1.625

fuselage/fuselage_data.scad

wing_post_color

WOOD_Balsa

fuselage/wing_post/wing_post_data.scad

wing_post_height

wing_elevation + tube_height

fuselage/wing_post/wing_post_data.scad

wing_rib_camber

4

math_magik_lpp_data.scad

wing_spar_size

1/16

math_magik_lpp_data.scad

wing_tip_radius

2

math_magik_lpp_data.scad

wing_x_offset

1.625

math_magik_lpp_data.scad

wire_diameter

0.025

fuselage/rear_hook/rear_hook_data.scad