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8976RS072PA6

Description
Rack and Panel Connector,
CategoryThe connector    The connector   
File Size225KB,5 Pages
ManufacturerEsterline Technologies Corporation
Download Datasheet Parametric View All

8976RS072PA6 Overview

Rack and Panel Connector,

8976RS072PA6 Parametric

Parameter NameAttribute value
MakerEsterline Technologies Corporation
Reach Compliance Codeunknown
ECCN codeEAR99
Connector typeRACK AND PANEL CONNECTOR
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).
108
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