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MIL-C-26482 Series II °è¿ÀÇ Ä¿³ØÅÍ´Â ´ç»çÀÇ ÃàÀûµÈ ±â¼ú·Î °³¹ßµÈ Ä¿³ØÅÍÀÔ´Ï´Ù.
¼ÒÇüÀ¸·Î Àü±â ÀüÀÚÀåºñ ¹× ȯ°æÀû Ư¼ºÀÌ ¿ì¼öÇÏ¿© °íµµÀÇ ½Å·Ú°¡ ¿ä±¸µÇ´Â Ç×°øÀåºñ ¹× ¹Ì»çÀϵî ÷´Ü Åë½ÅÀåºñµî¿¡ ³Î¸® »ç¿ëµÇ°í ÀÖ½À´Ï´Ù.
ƯÈ÷ ÀüÀÚÆÄ ÀåÇØ(EMI)¸¦ ¿Ïº®È÷ Â÷´Ü½ÃŰ¹Ç·Î ÀüÇô ¿ÜºÎ°£¼·À» ¹ÞÁö ¾Ê°í ¾ÈÁ¤ÀûÀÎ ½Ã±×³Î ¶óÀÎÀ» ±¸ÃàÇÒ ¼ö ÀÖ´Â°Ô ÀåÁ¡ÀÔ´Ï´Ù.
¶ÇÇÑ ÄÉÀ̺í ÀÛ¾÷½Ã °£´ÜÇÑ Å¬¸²ÇÎ Åø(Crimping Tool)·Î °á¼±ÀÌ °¡´ÉÇϹǷΠ³³¶«(Soldering)ÀÛ¾÷½Ã ¹ß»ýÇÒ ¼ö ÀÖ´Â ºÒ·®À» ¹æÁöÇϰí, ÀÛ¾÷½Ã°£ÀÇ ´ÜÃàÀÌ Å« ÀåÁ¡ÀÔ´Ï´Ù.
We developed the MIL-C-26482 Series II type connectors with our accumulated technology.
These small sized connectors are available for many applications, from the leading edge communication systems to the most stringent high reliability aerospace and missile requirements.
These connectors shield EMI completely, thus they provide a very stable signal lines without any interference.
Since the connector to cable is made by using simple crimping tool, the errors due to soldering can be avoided and the manufacturing efficiency is increased.
Ç×°ø±â, ÅÊÅ©, ¹Ì»çÀÏ, ÇÔÁ¤, Åë½Å½Ã½ºÅÛ, ÀÇ·á±â±â, ·Îº¸Æ® µî ÷´Ü »ê¾÷±â±â
Airplane, tank, missile, ship communication system, medical instrument, robot and high tech industry equipment.
A cross sectional diagram
¨ç contact insertion/extraction tool
¨è Hard Insulator
¨é Resilient Insulator
¨ê Contact ( +, - )
»ç¿ë¿Âµµ (Temperature range)
-65¡É to +175¡É
³»±¸¼º ( Durability)
ÃÖ¼Ò 500ȸ °áÇÕ ¹× ºÐ¸®.
minimum 500 mating and numating operations.
Ãæ°Ý°ú Áøµ¿ ( Shock and vibration)
½ÃÇè¿ä±¸¿¡ µû¶ó Ãæ°Ý°ú Áøµ¿½ÃÇè½Ã Àü·ù ºÒ¿¬¼ÓÀÌ 1ms ÀÌÇÏ¿©¾ß ÇÔ.
The current flows shall be suspended for any discontinuity of less than 1ms for the requirement of
shock and vibration test.
Ãæ°Ý ( Shock)
Ãæ°ÝÀº 300GÀÇ »çÀÎÆÄ Ãæ°ÝÀ» 3°÷ÀÇ Ãà¹æÇâÀ¸·Î 3millisecond µ¿¾È Àΰ¡ÇÑ´Ù.
The connectors shall be subjected to the shock in each of three mutually perpendicular axes.
The pulse shall be the since wave of impulse of 30G with a duration of 3 milliseconds
Áøµ¿ (Vibration)
·£´ýÁøµ¿À» Á֯ļö¹üÀ§ 50¿¡¼ 2000Hz¿Í 41.7GÀÇ ÃÖ»óÁ¡À» 16½Ã°£ °¡ÇÔ.
The duration shall be 16 hours for random vibration in the freq. ranges from 50§Ô to 2000§Ô at
maximum point of 41.7G.
Shell
Aluminum alloy
Electroless nickel MIL-C-26074,
Anodized per MIL-A-8625 or
olive drab cadmium over nickel
Insulators
Rigid dielectric
None
Elastomers
(grommets,
interfacial and
O-ring seals)
Silicone rubber or
Fluorosilicone rubber
None
Contacts
Copper alloy
Gold plating MIL-G-45204
Coupling Nut
Aluminum alloy
Electroless nickel per MIL-C-26074,
anodized per MIL-A-8625 or
olive drab Cadmuim over Nickel or
Zink over Nickel
Jam Nut
Aluminum alloy
Shell Types
MS Number
Designation
MS3470
Narrow Rlange Receptacle
MS3471
Cable Connecting Receptacle
MS3472
Wide Flange Receptacle
MS3474
Jam Nut Receptacle
MS3475
Straight Plug, RFI Shielded
MS3476
Straight Plug
Class
MS Class
Application
A
Fluid resistant, 200¡É, non-conductive(anodized)
L
Fluid resistant, 200¡É, conductive, finish(nickel)
W
Corrosive and fluid resistant, 175¡É(cadmium over nickel)
Shell Size
8, 10, 12, 14, 16, 18, 20, 22, 24
Contact Arrangement
See, MIL-STD-1669
Contact Style
P - PIN S - SOCKET
Alternate Insert Position
W. X. Y. Z. (Ref. : MIL-STD-1669)
Contact Current Rating and Retention
Contact size
Wire size
Max. Current
for Tests (amps)
Potential Drop
(Millivolts at 25¡É)
20
#20
7.5
55
#24
3.0
45
16
#16
13
50
#20
7.5
45
12
#12
23
50
#14
17
45
Voltage resistance
Altitude
Test voltage
ft.
I
II
Sea Level
1500
2,300
50,000
500
750
70,000
375
500
100,000
200
200
Admissible wire
Contact size
Inter diameter of contacting port
Wire size (AWG)
20
Ø 1.2
24, 22, 20
16
Ø 1.7
20, 18, 16
12
Ø 2.5
14, 12