65043-010LF Просмотр технического описания (PDF) - First Components International

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Компоненты Описание

производитель

65043-010LF

Basics+,Mini-PV™ : 2.54 x 2.54 mm (0.1 x 0.1 in.) Centerline Crimp-to-Wire PV Receptacle Housing, Double Row

First Components International 

TYPE

PRODUCT SPECIFICATION

NUMBER

BUS-12-067

TITLE

Crimp-to Wire, Mini-PV™ Receptacles and Mini-Latch Housings

PAGE

REVISION

11 of 16

K

AUTHORIZED BY

DATE

H.T. Brewbaker 31-May-06

CLASSIFICATION

UNRESTRICTED

7.8 Probe Damage - After testing in accordance with MIL-STD-1344, Method 2006, the individual contact

withdrawal force shall not be less than the value specified in Table III (see paragraph 7.5). The

following details shall apply:

a. Moment - 0.125 inch pounds (A= 0.025)

b. Probe Depth - To reach apex of spring

c. Stress Point - Contact spring member only

8.0 Environmental Conditions

After exposure to the following environmental conditions in accordance with the specified test procedure and/or

details, the product shall show no physical damage and shall meet the electrical and mechanical requirements

per paragraphs 6.0 and 7.0 as specified in the Table VI test sequences.

8.1 Thermal Shock - MIL-STD-202, Method 107, Unmated.

a. Temperature Range - Between -55 and + 105 deg C

b. Time at Each Temperature - Per sample mass

c. Transfer Time - 5 minutes, maximum

d. Number of Cycles - 5

8.2 Humidity - MIL-STD-1344, Method 1002, Type I, Unmated. Measurements taken within one hour of

removal from humidity chamber.

a. Test Temperature - + 40 +/- 2 deg C.

b. Test Duration - 96 hour

c. Test Relative Humidity - 90-95%

d. Test Condition - B

8.3 High Temperature Life - MIL-STD-1344, Method 1005, Mated.

a. Test Temperature - 3 ( +85 +/- 3 deg C)

b. Test Duration - B (250 hours)

c. Operating Conditions - rated current (see paragraph 6.1, Figure 1A) through all contacts

d. Duty Cycle - 45 minutes ON, 15 minutes OFF

8.4 Shock - MIL-STD-1344, Method 2004, Test Condition A, Mated. During and after each shock, the

contacts shall evidence no discontinuity greater than one microsecond.

8.5 Vibration - MIL-STD-1344, Method 2005, Test Condition III, Mated. During vibration along each axis, the

contacts shall evidence no discontinuity greater than one microsecond.

Copyright FCI

Form E-3334

Rev E

PDM: Rev:K

GS-01-001

STATUS:Released Printed: Nov 28, 2010.

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