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8976RM072SB6

产品描述Rack and Panel Connector,
产品类别连接器    连接器   
文件大小225KB,共5页
制造商SOURIAU
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8976RM072SB6概述

Rack and Panel Connector,

8976RM072SB6规格参数

参数名称属性值
厂商名称SOURIAU
Reach Compliance Codeunknown
ECCN代码EAR99
连接器类型RACK AND PANEL CONNECTOR

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MAXI-D Series
Connectors for
Astronaut Operations
In the frame of Space Station Alpha program, SOURIAU has developed and qualified a series
of Astronaut operable high reliability rectangular connectors which are suitable for both IVA
& EVA activities. This hardware is used on the COF (Colombus Orbital Facility) module which
is part of the European contribution to the Space Station. These connectors feature :
• Low Insertion Force contacts
• High density of contacts (72 # 22)
• Scoop proof design
• High durability (5000 mating/demating operations)
• High EMI shielding efficiency
• Associated dismountable EMI backshells
• Easy inspection, maintenance or repair after wiring.
Characteristics
Materials and finishes
Components
Shells & backshells
Inserts
- Insulator
- Wire guide
Contacts
Contact retaining clip
Locking device
- Mechanical parts
- Springs
Material
Aluminium alloy
Duroplastic
Silicone
See L.I.F. contacts
Copper alloy
Aluminium alloy
Stainless steel or Berylium copper
Finish
Nickel plating : electroless & flashing
-
-
See L.I.F. contacts
-
Electroless Electrolytic Nickel plated
-
Maximum ratings
1
2
3
4
5
6
Characteristics
Working voltage (sea level)
Rating current
Operating temperature range
Mating/Demating in mated status
Storage temperature range
Soldering temperature
Connector life
Symbol
U
r
I
r
T
op
T
stg
T
sol
---
Maximum ratings
min
Max.
---
---
-55
+15
-65
---
---
200
5
+150
+40
+150
+260
> 500
Unit
Vrms
A
°C
°C
°C
°C
cycles (1)
(1) 1 cycle = 1 mating/demating over 10 years
Electrical characteristics
1
2
3
4
Characteristics
Insulation resistance
Voltage proof - Leakage current
Mated shell conductivity
(1)
Contact resistance
Symbol
Ri
I
L
R
R
c
Test
method
Test
condition
Limits
min
10 000
---
---
---
Max.
---
2
7
6
Unit
MW
mA
mW
mW
ESA/SCC 3401
para. 9.1.1.1 para. 9.1.1.1
ESA/SCC 3401
800 Vrms
para. 9.1.1.2
ESA/SCC 3401
para. 9.1.1.4 para. 9.1.1.4
ESA/SCC 3401
para. 9.1.1.3 para. 9.1.1.3
(1) From grounding screw of the backshell to the receptacle flange.
(These measurements have been performed at :
Tamb = + 22 ± 3°C).
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