evaluation of press-fit connector for space-flight
TRANSCRIPT
TÜV NORD GROUP
EVALUATION OF PRESS-FIT CONNECTOR FOR SPACE-FLIGHT APPLICATIONS,
FEEDBACK AND DESIGN IMPROVEMENTS
2
Trends show an increasing demand for the incorporation of new fabricationconcepts and components into the space industry. This requires for fast andreliable evaluation processes adapted to the specific system design and thecharacteristics.
Press-fit technology is already consolidated in different industrial sectors andcurrently is emerging for space applications.
Solder-less alternative for PCB assembly.
Cost and time effective.
Mature commercial technologies
Space qualification
Spaceimplementation
This communication reports on thequalification process to asses the reliability ofselected press-fit connector for theimplementation in space applications.
INTRODUCTION
3
Standard and high density connectors comply with the
space regulation
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0020.00 100.00 1000.00
8.3176
0.0013
0.0100
0.1000
1.0000
Frequency (Hz)
(gn)²/Hz
-80
-60
-40
-20
0
20
40
60
80
100
120
0:0
00:1
50:3
00:4
51:0
01:1
51:3
01:4
52:0
02:1
62:3
12:4
63:0
13:1
63:3
13:4
64:0
14:1
74:3
24:4
75:0
25:1
75:3
25:4
76:0
26:1
86:3
36:4
87:0
37:1
87:3
37:4
88:0
38:1
8
TEM
PER
AT
UR
E
(ºC
)
TIME (minutes)
Vibrationand temperature cycling
Control visual inspections Control electrical
measurements
Microsectioning Microinspection
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
PCB 1 Conect. 1 PCB 2 Conect. 1 PCB 3 Conect. 1
Aver
age
Cont
act R
esita
nce
(mΩ
)
Initial Vibration 200 Temp Cycles 300 Temp Cycles
Thorough and accurate tests are conducted to determine thesuitability for space applications
Environmental test
4
1. Compliant-Press-Fit concept
2. Test vehicles and test flow
3. Vibration test
4. Temperature cycling
5. Visual inspection and electrical verification control test
6. Micro section inspection
7. 2nd Generation
8. Summary
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
PCB 1 Conect. 1 PCB 2 Conect. 1 PCB 3 Conect. 1
Aver
age
Cont
act R
esita
nce
(mΩ
)
Initial Vibration 200 Temp Cycles 300 Temp Cycles
-80
-60
-40
-20
0
20
40
60
80
100
120
0:0
00:1
50:3
00:4
51:0
01:1
51:3
01:4
52:0
02:1
62:3
12:4
63:0
13:1
63:3
13:4
64:0
14:1
74:3
24:4
75:0
25:1
75:3
25:4
76:0
26:1
86:3
36:4
87:0
37:1
87:3
37:4
88:0
38:1
8
TEM
PER
AT
UR
E
(ºC
)
TIME (minutes)
OUTLINE
5
Deformable tail is inserted into a plate
through hole (PTH).
PTH slightly narrower than theinsertion pin.
Eye-of-the-needle design: The tail isadapted to the PTH at the same timethat the spring-force ensurespermanent low-resistivity electricalcontact.
Semiautomatic mounting tool to regulatethe insertion force.
COMPLIANT-PRESS-FIT CONCEPT
6
Denomination Pin size Number of pins Intended aplication Quantuty
High density 22 75 Singal comunication 3 PCBs with 2 connectors
Standard density 20 50 Low power supply 3 PCBs with 2 connectors
Combo-D 8 5 High power supply 3 PCBs with 2 connectors
General PCB characteristics
- 4 Cu layers of 2.4 mm of thickness - Electroless Nickel Immersion Gold (ENIG) - PTHs gold coating of 5 µm of thickness
3 types of press fit connectors conceived for different applications:
Signal communication. Low power supply. High power supply.
High density75 pins Standar density
50 pinsCombo-D
8 pins
TEST VEHICLES
Inspections
Environmental tests
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
7
Qualification program adapted from ECSS-Q-ST-70-38C for surface mounting technology but including harder requirements
Test / inspection Specification
Visual inspection ESCC 20500
Electrical characterization DENG-008-1 Rev. B § 7 (customer procedure)
VibrationECSS Q ST 70 08C § 13 (sine + random)
Additional provision µ-cuts ≥ 1 µs are not allowed
Temperature Cycling
DENG-008-1 Rev. B Par. 14
-55 ºC to +100 ºC abrupt thermal shock
Cross-section µ-inspection DENG-008-1 Rev. B
TEST FLOW
8
Vibration
Inspections
Environmental tests
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
9
Sine sweep vibration test Random vibration test
High level vibration
High level vibration
XAxis
YAxis
ZAxis
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(Y)
Sine Sweep
(Y)
Sine survey
(Y)
Sine survey
(Z)
Sine Sweep
(Z)
Sine survey
(Z)
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Random(X)
Sine survey
(X)
Sine survey
(Y)
Random(Y)
Sine survey
(Y)
Sine survey
(Z)
Random(Z)
Sine survey
(Z)
VIBRATION TEST: TEST SEQUENCE
10
DUT natural frequencies identification
High level vibration
DUT natural frequencies
shift
In situ electrical
monitoring
Electrical
Electrical discontinuities
(in-situ)
Resistance drift (ex-situ)
Mechanical
Natural frequencies
(in-situ)
Visible damages (ex-situ)
Inspected parameters
In-situ inspection
Sine sweep and random vibration tests
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Sine orrandom
(X)
Sine survey
(X)
Sine survey
(Y)
Sine orrandom
(Y)
Sine survey
(Y)
Sine survey
(Z)
Sine orrandom
(Z)
Sine survey
(Z)
VIBRATION TEST: INSPECTED PARAMETERS
11
Y-axis vibration
Vibr
atio
n
Z-axis vibration
X-axis vibration
Elec
trica
l m
onito
ring
Daysi chain electrical monitoring
VIBRATION TEST: SET-UP
No discontinuities longer than 1 µs were observed
12
High level vibration
Sine Sweep conditions
Range Amplitude(0 to peak) Sweep rate
25 to 100 Hz 20 g 1 oct/min
100 to 200 Hz 15 g 1 oct/min
Vibration level follows the required profile neither resonances nor other deviations were observed
In situ electrical
monitoring
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(Y)
Sine Sweep
(Y)
Sine survey
(Y)
Sine survey
(Z)
Sine Sweep
(Z)
Sine survey
(Z)
VIBRATION TEST: SINE SWEEP
13
Sine sweep vibration test Random vibration test
High level vibration
XAxis
YAxis
ZAxis
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(Y)
Sine Sweep
(Y)
Sine survey
(Y)
Sine survey
(Z)
Sine Sweep
(Z)
Sine survey
(Z)
Sine Sweep
(X)
Sine survey
(X)
Sine survey
(X)
Random(X)
Sine survey
(X)
Sine survey
(Y)
Random(Y)
Sine survey
(Y)
Sine survey
(Z)
Random(Z)
Sine survey
(Z)
VIBRATION TEST: RANDOM
14
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0020.00 100.00 1000.00
8.3176
0.0013
0.0100
0.1000
1.0000
Frequency (Hz)
(gn)²/Hz
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0020.00 100.00 1000.00
3.1623
0.0126
0.1000
1.0000
Frequency (Hz)
(gn)²/Hz Parallel to PCB
Range (Hz) PSD level
20 to 100 +3 dB/oct (ramp)
100 to 800 0.5 g2/Hz (plateu)
800 to 2000 -3 dB/oct (ramp)
Global RMS 27.1
Vibration level confined within the required range. Neither resonances nor other deviations were observed
Perpendicular to PCB
Range (Hz) PSD level
20 to 100 +6 dB/oct (ramp)
100 to 500 1 g2/Hz (plateau)
500 to 2000 -6 dB/oct (ramp)
Global RMS 28.5
No discontinuities longer than 1 µs were observed
VIBRATION TEST: RANDOM
Sine survey
(X)
High level
vibration(X)
Sine survey
(X)
Sine survey
(X)
High level
vibration(X)
Sine survey
(X)
Sine survey
(X)
High level
vibration(X)
Sine survey
(X)
Sine surveyNatural frequencies analysis
Test conditionsAmplitude 0.5 g (0 to peak)Frequency 10 to 2000 HzSweep rate 2 oct/min
Direction X, Y & Z
DUT natural frequencies identification
DUT natural frequencies identification
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
VIBRATION TEST: NATURAL FREQUENCIES
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
X-Ax
isY-
Axis
Z-Ax
is
Initial After high level vibrationAfter high level
vibration
(sine sweep and random)
The DUT preserves its mechanical impedance.
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
profile(f)
high-abort(f)
low-abort(f)
high-alarm(f)
low-alarm(f)
control(f)
2000.0010.00 100.00 1000.00
1.1749
0.1778
1.0000
Frequency (Hz)
gn
No changes on the DUT
natural frequencies are observed
VIBRATION TEST: NATURAL FREQUENCIES
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
17
Inspections
Environmental tests
Temperature cycling
High temperature 100 ºC
Low temperature - 55 ºC
Soak time 15 min
ESA speciation for soldered connections imposes temperature ramps < 10 ºC/min
According to the customer specifications harder conditions were applied.
-80
-60
-40
-20
0
20
40
60
80
100
120
00:0
0
00:0
2
00:0
5
00:0
8
00:1
1
00:1
4
00:1
7
00:2
0
00:2
3
00:2
5
00:2
8
00:3
1
00:3
4
00:3
7
00:4
0
00:4
3
TEM
PER
ATU
RE
(ºC
)
Stabilization time < 10 min
DU
TH
ot b
ath
Col
d ba
th
Thermal shock between two air baths.
TEMPERATURE CYCLING: SET-UP AND CONDITIONS
-80
-60
-40
-20
0
20
40
60
80
100
120
00:0
000
:15
00:3
000
:45
01:0
001
:15
01:3
001
:45
02:0
002
:16
02:3
102
:46
03:0
103
:16
03:3
103
:46
04:0
104
:17
04:3
204
:47
05:0
205
:17
05:3
205
:47
06:0
206
:18
06:3
306
:48
07:0
307
:18
07:3
307
:48
08:0
308
:18
TEM
PER
ATU
RE
(ºC
)
TIME (minutes)
PCB ComboDS/N 0
ComboDS/N 1
ComboDS/N 2
Standard S/N 0
Standard S/N 1
Standard S/N 2
High S/N 0
High S/N 1
High S/N 2
Min -57.0 -56.6 -56.7 -57.0 -57.0 -56.8 -57.0 -57.0 -57.0
Max 101.2 102.4 100.6 102.1 101.9 103.0 102.7 102.3 102.8
Temperature register of 10 representative
cycles
To ensure the test reliability the temperature is continually monitored withISO17025-calibrated thermocouples attached to the DUT surface.
Max and min temperatures are within the tolerances stated by MIL-STD-202 TM107
TEMPERATURE CYCLING: SET-UP AND CONDITIONS
20
Inspections
Environmental tests
Visual inspection
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
21
In one case small marks were observed near the PTH after mounting and unmounting test.
No evolution was observed after each environmental test
For most of inspected connectors and PCB no noticeable deviations were observed
VISUAL INSPECTION
22
Inspections
Environmental tests
Electrical verification
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
0
0.2
0.4
0.6
0.8
1
1.2
PCB 1Conect. 1
PCB 1Conect. 2
PCB 2Conect. 1
PCB 2Conect. 2
PCB 3Conect. 1
PCB 3Conect. 2
Aver
age
Con
tact
Res
itanc
e (m
Ω)
Initial Vibration 200 Temp Cycles 300 Temp Cycles
0
0.2
0.4
0.6
0.8
1
1.2
PCB 1 0º PCB 1 90 º PCB 2 0º PCB 2 90 º PCB 3 0º PCB 3 90 º
Combo D
Standard
0
0.2
0.4
0.6
0.8
1
1.2
PCB 1 0º PCB 1 90 º PCB 2 0º PCB 2 90 º PCB 3 0º PCB 3 90 º
Aver
age
Con
tact
Res
itanc
e (m
Ω) High
In all the cases R < 1 mΩ no variations of statistical
significance were observed
VISUAL INSPECTION
24
Inspections
Environmental tests
Microsectioning
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
25
µ-se
ctio
ning
Visu
al &
fluo
resc
ent
µ-in
spec
tion
Selected parts are separated from PCB & cut using a precision diamond wire saw.
Each sample placed in a mounting mold & embedded into epoxy resin (low exothermic).
Luminescent marker added to the resin to analyse defects using its fluorescence.
Automatic Grinding/polishing machine.
Normal and/or fluorescent micro-inspection
MICROSECTIONING & MICROINSPECTIONAccurate wire cutting
Cold Mounting suitable for sensitive parts Multi-step delicate
gridding & polishing
26
Control the removalrate depending onPressure, Time &Rotational Speed.
Damages reductionproduced by the grindingprocess.
Gridding and Polishing optimization by DOE methodology.
Results presented at the Electronic Materials and Processes for Space 9th Workshop, YVERDON-LES-BAINS
Optimization
Certifications
Certified inspectors:
Inspection of crimping connections (ECSS-Q-ST-70-26)Inspection of solder joints for SM & mixed technology (ECSS-Q-ST-70-38).
To be announced:
ESA Recommended company for PCB assembly verifications (ECSS-Q-ST-70-38).
In progress: ISO17025 certification to conduct PCB verification programmes (ECSS-Q-ST-70-38)
Original
27
Through and an detailed inspection in different inspection planes
Transversal cut right connector
Transversal cut vertical connector
Longitudinal cut vertical connector
Stan
dard
and
hig
h de
nsity
con
nect
ors
Com
bo-D
co
nnec
tors
Transversal cut vertical connector
Longitudinal cut vertical connector
MICROSECTIONING & MICROINSPECTION
28
Cracks: • Base of the pin insert • PCB resin
No other anomalies are observed
Combo-D connectors
MICROSECTIONING & MICROINSPECTION
30
Standard and high density Environmental µ-inspection
Visual +
Electrical
Detailed µ-inspection enables Positronic to identify the trouble and develop new design to overcome the observed issues
Combo-D
Standard and high density connectors successfully pass all the tests
1ST GENERATION SUMMARY
Connector mountingon PCB
Visual inspection+
Electrical verification
Connector unmounting
from PCBx1
Visual inspection+
Electrical verification
VibrationTests (sin + random)
Visual inspection+
Electrical verification
Temperature cycling200 cycles
Visual inspection+
Electrical verification
Cross-sectionInternal µ-inspection
Temperature cycling300 cycles
Visual inspection+
Electrical verification
31
Environmental test
Inspection
In some cases initial external visual inspection revealed anomalies (crazing) at the PCB.
Environmental testAll the inspected specimens
successfully pass the environmental tests and the
electrical verifications.
Microsection inspectionDissimilar results. Further developments in progress.
2ND GENERATION SUMMARY
SUMMARY.
• Different types of press-fit connectors conceivedfor different applications has been assesses fortheir implementational in space environments.
• The verification program included:
o Hard environmental (vibration andtemperature cycling) tests.
o Control electrical and visual inspections.o Detailed microsection inspections.
• Standard and high density connectorssuccessfully passed all the tests andinspections , demonstrating high reliability andassembly consistency.
• Combo-D presented internal cracks as revealedby µ-inspection.
• New Combo-D are under developed indenting toovercome such shortcoming.
Mature commercial technologies
Space qualification
Spaceimplementation
TÜV NORD GROUP
THANK YOU FOR YOUR KIND ATTENTION!
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