MS21433F
Inches |
mm |
Inches |
mm |
Inches |
mm |
||
.003 .004 .005 .015 .024 .025 |
0.08 0.10 0.13 0.38 0.61 0.64 |
.045 .048 .067 .093 .100 .110 |
1.14 1.22 1.70 2.36 2.54 2.79 |
.125 .160 .170 .200 .205 .210 |
3.18 4.06 4.32 5.08 5.21 5.33 |
.250 .364 .420 .440 .500 .572 |
6.35 9.25 10.67 11.18 12.70 14.53 |
NOTES:
1. Dimensions are in inches.
2. Metric equivalents are given for general information only.
3. Unless otherwise specified, tolerances are ±.010 (0.25 mm) on decimals and ±5° on angles.
4. Terminals need not be marked. Terminal identification is shown for reference purposes only.
FIGURE 1. Dimensions and configuration - Continued.
REQUIREMENTS:
For hardware detail specifications, see appendix of MIL-DTL-8834.
In the event of a conflict between the text of this specification and the references cited herein, the text of this specification shall take precedence.
Shock: Method I and method II (high impact). The switches shall be rigidly mounted to the shock test equipment by means of their terminals and mounting tab. The switch shall be electrically and mechanically operative at the conclusion of the test and there shall be no mechanical transfer during the test.
Terminals: Gold plated.
Weight: .0165 pound maximum (6.15 grams).
Strength of terminals: Terminals shall be subjected to a five-pound pull for 5 to 10 seconds with the long dimension of the terminal contact vertical. The force shall be applied to the terminal at a point .06 inch (1.5 mm) below the bottom of the switch base, and in a direction parallel to the axis of the toggle lever in its center
position. Two outboard terminals shall be tested. However, a terminal shall be tested only once in one direction.
Altitude: 50,000 feet.
Strength of actuator. Lever pivot and lever stop 6 pounds. Mounting bracket: Brass, tin plated, or coated.
For hardware detail specifications, see appendix of MIL-DTL-8834.
2
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