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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.

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MIL-STD-2066(AS)
TABLES (Continued)
Page
Table
C13-1 Constant Pressure Catapult (CVAN68), Upper Boundary,
30
52
Load vs Stroke, Numerical ............................
C13-1 Constant Pressure Catapult (CVAN68), Mean,
31
53
Load vs Stroke, Numerical ...........................
C13-1 Constant Pressure Catapult (CVAN68), Lower Boundary,
32
54
L o a d v s S t r o k e , N u m e r i c a l ................................
C E 1 - 3 Catapult (capacity operation), Load vs Stroke,
33
55
Nondimensional ...........................................
11
C 7 Catapult Tow Force vs Stroke for a 45,000 Pound Airplane
34
Calculation of the CE1-3 Catapult Tow Force vs Stroke for a
35
13
37,685 Pound Airplane . . . . . . . . . . . . . .
36
List of Figures Showing Nondimensional Load vs Stroke Curves
14
f o r Specific Airplane Weights and Arresting Gears .........
37
Calculation of Peak Nondimensional Load for a 17,500 Pound
18
Airplane.....................................................
19
Load-Stroke Values for a 17,500 Pound Airplane . . . . . . . . . . . . . . .
38
21
A d j u s t m e n t of Cycles per Interval .............................
39
40
Calculation of Peak Nondimensional Load for a 45,000 Pound
24
Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .



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