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MIL-STD-2066 Catapulting And Arresting Gear Forcing Functions For Aircraft Structural Design \(S/S By Mil-Hdbk-2066\)The information contained herein presents loading characteristics, associated parameters, and methods to be used in calculating the catapulting and arresting loads of MIL-A-8863 and MIL-A-8866 for the design of U.S. Navy airplanes operating from shipboard and shorebased launching and recovery gears. A listing of such gears for which data is contained herein is given in Table 1.

Pages 1 - 2 - 3 - 4 - 5 - 6 - 7 - 8 - 9 - 10


MIL-STD-2066(AS)
FIGURES (Continued)
Page
Figure
123
17.2
MK7-2 Gear, Correction Factor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17.3
MK7-2 Gear, Average Frequency and Amplitude of Oscillation,
129
Nondimensional . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
130
17.4
MK7-2 Gear, Maximum Peak Arresting Force . . . . . . . . . . . . . . . . . . . . . .
131
MK7-2 Gear, Mean Peak Arresting Force . . . . . . . . . . . . . . . . . . . . . . . . .
17.5
132
MK7-3 Gear, 10,000 Lb Weight, Load vs Stroke, Nondimensional . .
18.1
133
18.2
MK7-3 Gear, 15,000 Lb Weight, Load vs Stroke, Nondimensional . .
134
18.3
MK7-3 Gear, 20,000 Lb Weight, Load vs Stroke, Nondimensional . .
135
MK7-3 Gear, 30,000 Lb Weight, Load vs Stroke, Nondimensional . .
18.4
136
MK7-3 Gear, 40,000 Lb Weight, Load vs Stroke, Nondimensional . .
18.5
137
MK7-3 Gear, 50,000 Lb Weight, Load vs Stroke, Nondimensional . .
18.6
138
18.7
MK7-3 Gear, 60,000 Lb Weight, Load vs Stroke, Nondimensional . .
139
19.1
MK7-3 Gear, Limit Engaging Speed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
140
19.2
MK7-3 Gear, Correction Factor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
19.3
MK7-3 Gear, Average Frequency and Amplitude of Oscillation,
141
Nondimensional......................................................
142
19.4
MK7-3 Gear, Maximum Peak Arresting Force . . . . . . . . . . . . . . . . . . . . . .
143
19.5
MK7-3 Gear, Mean Peak Arresting Force . . . . . . . . . . . . . . . . . . . . . . . . .
144
20.1
M-21 Gear, 10,000 Lb Weight, Load vs Stroke, Nondimensional . . .
145
20.2
M-21 Gear, 15,000 Lb Weight, Load vs Stroke, Nondimensional . . .
146
20.3
M-21 Gear, 20,000 Lb Weight, Load vs Stroke, Nondimensional . . .
20.4
147
M-21 Gear, 30,000 Lb Weight, Load vs Stroke, Nondimensional . . .
148
M-21 Gear, 40,000 Lb Weight, Load vs Stroke, Nondimensional . . .
20.5
149
20.6
M-21 Gear, 50,000 Lb Weight, Load vs Stroke, Nondimensional . . .
20.7
150
M-21 Gear, 60,000 Lb Weight, Load vs Stroke, Nondimensional . . .
151
21.1
M-21 Gear, Limit Engaging Speed ........................
152
21.2
M-21 Gear, Correction Factor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
21.3
M-21 Gear, Average Frequency and Amplitude of Oscillation,
Nondimensional . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
153
154
M-21-Gear, Maximum Peak Arresting Force (Dry Tapes) ........
21.4
M-21 Gear, Mean Peak Arresting Force (Dry Tapes) . . . . . . . . .
21.5
155
21.6
M-21 Gear, Runout to be Used in Dimensioning Load-Stroke Data .
156
M-21 Gear, Wet Tape Correction Factor . . . . . . . . . . . . . . . . . . . . . . . . .
21.7
157
M-21 Gears Maximum Peak Arresting Force (Wet Tapes) ...........
21.8
158
E-15 Gear, 10,000 Lb Weight, Load vs Stroke, Nondimensional . .
22.1
159
22.2
E-15 Gear, 15,000 Lb Weight, Load vs Stroke, Nondimensional . . .
160
E-15 Gear, 20,000 Lb Weight, Load vs Stroke, Nondimensional ..
22.3
161
22.4
162
E-15 Gear, 30,000 Lb Weight, Load vs Stroke, Nondimensional . . .
E-15 Gear, 40,000 Lb Weight, Load vs Stroke, Nondimensional . . .
22.5
163
22.6
E-15 Gear, 50,000 Lb Weight, Load vs Stroke, Nondimensional . . .
164
22.7
E-15 Gear, 60,000 Lb Weight, Load vs Stroke, Nondimensional . . .
165
23.1
E-15 Gear, Runout to be Used in Dimensioning Load-Stroke Data .
166
E-15 Gear, Span Conversion Factor . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
23.2
167
23.3
E-15 Gear, Average Frequency and Amplitude of Oscillation,
Nondimensional . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
168
23.4
E-15 Gear, Maximum Peak Arresting Force . . . . . . ................
169
23.5
E-15 Gear, Mean Peak Arresting Force . . . . . . . . . . . . . . . . . . . . . . . . . .
170
24
Base Thrust, SATS Arrestments . . . . . . . . . . . . . . . . . . . . .
171
25
Load Stroke Curve for a 17,500 Lb Airplane . . . . . . . . . . . . . . . . . . . .
23
viii



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