3
Blackhawk AGM-84 Standard ARM
1
0.75
0.8
0.81
0.95
0.95
1
0.
0.
0.
0.
0.
0.
0.
0.
1
914.4
0
0
0
1
0
Based on actual dimensions of completed model. Both sets of fins have thru the wall tabs to the motor tube
as defined by the centering rings. The two sections of body tubes are coupled with a tube coupler and
the tube coupler is glued to both. The original design called for a bulkhead 0.5 inches from the rear of the tube
coupler with an eye bolt for shock cord connection, the coupler glued to the forward payload section and slip
fit into the rear body tube. This design was not adapted as it allows approx. 8 inches of the side strake fins to
be exposed when the payload section separates from the rear body tube. A U-bolt in the forward motor mount
centering ring is used for shock cord retention via a quick link connector. Fins are beveled on all edges except
where attached to body tube.
Revised 1/21/06 - Change motor mount tube from 54mm to 38mm
1
26
1
0
CSV1|1|873.76,-9.9476e-14,0|700.656,-1841.33,-511.424|-0.169008,0.278485,-0.945454|1278,2730.21|30|2|1918.86|-8.22341|0|0|0|0
0,1377.81,0,0
0,18.7307,0,0
0,1407.51,0,0
0,25.543,0,0
0
1
0
1
0.
0.
0
0
0
0
5
0
0
0
0.
9.99998
9.99998
9.99998
9.99998
18
1
0.
0.
0
0.
0.
0.
0.
-1
Public Missiles
283.495
1049.21
Polystyrene PS
Nose cone
228.6
1
0.
389.499
320.204
0.0915715
0.0915715
0.
0
PNC-3.90
Plastic nose cone
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
1
0
0
0
blue
2.
0.198217
2.
0.198217
1
0
8
426.72
101.6
0
1
1
76.2
3.175
4.2
98.552
0.
0.
0.
LOC/Precision
0.
1121.29
Paper
Body tube
0.
0
0.
182.413
203.2
0.129717
0.129717
0.
0
LOC BT-3.9
Airframe tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
2
1
0
0
blue
0.
0.
0.
0.
1
0
8
101.6
99.06
406.4
0
0
0.
0.5
0.
0.
0
Public Missiles Ltd.
73.7088
1121.29
Paper
Tube coupler
0.
1
317.5
93.1
88.9
0.
0.
0.
0
CT-3.90
Coupler tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
16
0
0
0
blue
0.
0.
0.
0.
1
0
8
99.06
96.012
177.8
0
4
1
LOC Precision
142.
0.
Rip stop nylon
Parachute
0.
1
127.
22.032
122.5
0.
0.
0.
0
LP-58
58 In. 16 lines
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
18
0
0
0
blue
0.
0.
0.
0.
1
0
8
1470.
0.
0
16
0.051054
1350.
1
0.00102
1/16 In. braided nylon
0.75
LOC/Precision
0.
1121.29
Paper
Body tube
0.
0
0.
410.43
457.2
0.291864
0.291864
0.
0
LOC BT-3.9
Airframe tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
3
1
0
0
blue
0.
0.
0.
0.
1
0
8
101.6
99.06
914.4
0
0
0.
0.5
0.
0.
0
Custom
0.
344.269
1/4 Aircraft Plywood
Fin set
0.
0
0.
158.085
83.4746
0.0289245
0.115698
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
14
0
0
2
blue
13.4032
1.64613
18.4981
1.64634
1
0
8
4
158.75
20.65
139.62
140.226
82.07
6.35
2
0
0
120.65
29.972
19.05
1
0.
104.37
20.645
158.75,0|133.352,108.294|63.583,139.619|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Custom
0.
344.269
1/4 Aircraft Plywood
Fin set
0.
0
228.6
341.204
466.693
0.0690939
0.276376
0.
0
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
15
0
0
2
blue
3.32756
1.006
5.04488
1.01121
1
0
8
4
793.75
443.8
53.98
108.791
269.43
6.35
2
0
0
149.225
29.972
603.25
1
0.
636.36
443.8
793.75,0|742.811,53.8966|244.475,53.975|210.159,25.3884|31.6081,25.3884|0,0|
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
0,0,0,0,0,0,0
10,10,10,10,10,10,10
0,0,0,0,0,0,0
0.5,10,0.5,0.5,0.00018939,0.001,1
0.25,5,0.1,0.1,0.00018939,0.001,1
Public Missiles
0.
8553.86
Brass
Launch lug
0.
0
304.8
17.4265
76.2
0.00868415
0.00456037
0.
0
LL-0.38
55.5625
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
19
0
0
0
blue
0.
0.
0.
0.
1
0
8
9.525
8.5852
152.4
0
LOC/Precision
0.
1121.29
Paper
Body tube
0.
0
457.2
98.5033
228.6
0.
0.
0.
0
LOC MMT-1.52
Motor mount tube
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
7
1
0
0
blue
0.
0.
0.
0.
1
0
8
41.656
38.608
457.2
0
1
38.
12.7
0.
0.
1
LOC Precision
0.
724.996
Aircraft plywood (LOC)
Centering ring
0.
0
12.7
17.7405
1.5875
0.
0.
0.
0
LOC CR-3.9-2.14
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
8
0
0
2
blue
0.
0.
0.
0.
1
0
8
99.06
57.404
3.175
0
0
0
LOC Precision
0.
724.996
Aircraft plywood (LOC)
Centering ring
0.
0
139.7
17.7405
1.5875
0.
0.
0.
0
LOC CR-3.9-2.14
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
9
0
0
2
blue
0.
0.
0.
0.
1
0
8
99.06
57.404
3.175
0
0
0
LOC Precision
0.
724.996
Aircraft plywood (LOC)
Centering ring
0.
0
263.525
17.7405
1.5875
0.
0.
0.
0
LOC CR-3.9-2.14
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
10
0
0
2
blue
0.
0.
0.
0.
1
0
8
99.06
57.404
3.175
0
0
0
LOC Precision
0.
724.996
Aircraft plywood (LOC)
Centering ring
0.
0
419.1
17.7405
1.5875
0.
0.
0.
0
LOC CR-3.9-2.14
Centering Ring
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
11
0
0
2
blue
0.
0.
0.
0.
1
0
8
99.06
57.404
3.175
0
0
0
Public Missiles
76.5437
0.
6/7.5/11in. FNC Ubolt
419.1
1
419.1
0.
0.
0.
0.
0.
0
HDWE-UBOLT-SET
Ubolt for FNCs
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
23
0
0
2
blue
0.
0.
0.
0.
1
0
8
0
0.
LOC Precision
102.058
0.0167418
9/16 In. tubular nylon
Shock cord
0.
1
0.
0.
0.
0.
0.
0.
2
SCTN-20
Tubular Nylon 9/16 In x 20 Ft
0.
0.
file=()|position=(0,0,0)|origin=(0.5,0.5,0.5)|scale=(1,1,1)|repeat=(1)|interpolate=(0)|flipr(0)|flips(0)|flipt=(0)|preventseam=(1)
1.
0.
1.
0.
1.
blue
blue
white
1
24
0
0
0
blue
0.
0.
0.
0.
1
0
8
0
6096.
690.728
147.814
151.925
10.9638
8.7625
1
12.5717
683.408
10
12.2
2
2.20125
129.98
12.2
0.73671
147.441
3.47386
151.925
1.89234
295.796
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
3
1.34112
3.53163
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[I211W-10]
14.9133
0.
0.
0.115
1.86125
0.00125
800.
0
Earth
Standard earth condistions.
5.609
295.796
7.78589
3.47386
-6.96795
0,0,12.2,0,0
-1,-1,-1,-1,-1
0,0,12.2,0,0
32,32,80,32,32
1.
1
2.37982
1.12417
0.766195
0.0044995
18
1
0.
0.
1
683.408
12.5717
-65.3425
12.2
128
1
I211W
0.
Aerotech
12.7
0.
7
10.
852.199
187.443
187.217
11.6
9.79875
1
4.37187
852.002
10
11.8
2
1.80125
144.347
11.8
0.547825
187.195
2.07928
187.217
2.15959
155.9
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
3
1.34112
3.53163
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[I284W-10]
17.413
0.
0.
0.10125
1.565
0.00125
800.
0
Earth
Standard earth condistions.
3.829
155.9
6.86487
1.34524
-6.73177
0,0,11.8,0,0
-1,-1,-1,-1,-1
0,0,11.8,0,0
32,32,80,32,32
1.
1
2.47132
1.1377
0.771209
0.00578316
18
1
0.
0.
1
852.002
4.37187
-54.0014
11.8
128
1
I284W
0.
Aerotech
12.7
0.
7
10.
1033.18
220.209
257.242
12.2863
10.385
1
5.66036
1032.35
10
11.9
0
1.90125
201.48
11.9
0.387492
220.063
3.53138
257.242
5.26064
517.407
0.
0.
914.4
0
0.
0
0.
759.813
1.571
50.
15.
0.
0
3
1.34112
3.53163
2
0.01
0.02
0
5
0.
0.1
1
0.
0
3
300.
2000.
1
5.99999
2
0.99
2000.
1500.
2
0.98
1
0.
0
0.08
1
0.
1
0.
1
0.
[J350W-10]
20.7937
0.
0.
0.08625
1.50375
0.00125
800.
0
Earth
Standard earth condistions.
5.141
517.407
6.40141
3.53138
-5.33923
0,0,11.9,0,0
-1,-1,-1,-1,-1
0,0,11.9,0,0
32,32,80,32,32
1.
1
2.63925
1.16009
0.917669
0.00752365
18
1
0.
0.
1
1032.35
5.66036
-43.5006
11.9
128
1
J350W
0.
Aerotech
12.7
0.
7
10.