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WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006 page 1 Characterisation of high bandwidth 0.8μm laser diodes at EADS-ASTRIUM WORKSHOP Laser diodes in Space CNES – 12 mai 2006

06-01- Characterisation of high bandwith 0.8 um laser

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Page 1: 06-01- Characterisation of high bandwith 0.8 um laser

WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006page 1

Characterisation of high bandwidth 0.8µm laser diodes at EADS-ASTRIUM

WORKSHOP Laser diodes in SpaceCNES – 12 mai 2006

Page 2: 06-01- Characterisation of high bandwith 0.8 um laser

page 2 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

Content

1. Current 0,8 µm optical link : SILEX, LOLA

2. Product evolution

3. Future applications of 0,8 µm optical link

4. Need for European laser diode manufacturer

5. Lumics laser diode for LOLA demonstrator

6. Lumics laser diode improvements for increased bandwidth

7. High bandwidth Lumics laser diode

8. First characterisation results

9. Conclusion

Page 3: 06-01- Characterisation of high bandwith 0.8 um laser

page 3 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

1. Current 0,8 µm optical link : SILEX program

� Operational System used everyday

� More than 1200 successfull links between SPOT4 and ARTEMIS (with quasi error free quality)

� About 200 links with the ground

� Interoperability validated with theJaponese Luce terminal

278 liaisons optiques

en 2003

Etoile (Sirius, Arcturus , Betelgeuse )

OGS aux Iles Canaries

Artemis à 36000 km

Spot4 @ 830 km

More than 1000 optical links

Stars (Sirius, Arcturus , Betelgeuse )

OGS in The Canarian Islands

Artemis at 36000 km

Spot4 at 830 km

SILEX IN ORBIT SUCCESS

Page 4: 06-01- Characterisation of high bandwith 0.8 um laser

page 4 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

Current 0,8 µm optical link : LOLA PEA

� Customer: DGA

� Prime: Astrium / responsible for communication equipments: AAS

� Demonstration of a real time linkbetween an airplane and theground through a satellite

� Objective is to characterise theperformance of bi-directional linkbetween the airplane and Artemis

– with atmosphere perturbation

(turbulence, clouds, …)

– Dynamical perturbation of the

platform

� Planning : flights are plannedstarting summer 2006 until march2007

ARTEMIS

Effets

Nuages haute altitude

TurbulencesAtmosphériques

Aéro optiques

Émission diffuse

ARTEMIS

Page 5: 06-01- Characterisation of high bandwith 0.8 um laser

page 5 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

Link and propagation channel modellingCorrelation with OGS down link

Good correlation between channel modeldevelopped by Astrium in the frame of LOLA program on OGS link

Although this disturbing channel simulation show that transmission through atmosphere isachieved with direct detection at 0,8 µm

Page 6: 06-01- Characterisation of high bandwith 0.8 um laser

page 6 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

2. Product evolution at Astrium

1997OMNIS

1997OMNIS

1998OMNIX

1998OMNIX

1994SILEX

1994SILEX

1995SOUT

1995SOUT

Hemispherical pointing for LEO – GEO link

Terminal Mass Data Rate DistanceSILEX 158 Kg 50 Mbits/s 45.000 KmSOUT 50 Kg 50 Mbits/s 45.000 KmOMNIS 30 Kg 2400 Mbits/s < 4.000 KmOMNIX 20 Kg 150 Mbits/s < 7.000 Km

Page 7: 06-01- Characterisation of high bandwith 0.8 um laser

page 7 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

New optical terminals at Astrium : current design

LOLA LIO UAV

Terminal Mass Data rate DistanceLOLA - 50 Mbits/s 45 000 KmLIO LEO 36 Kg 2 x 300 Mbits/s 45 000 KmLIO GEO 45 Kg 3 x 300 Mbits/s 45 000 KmUAV 65 Kg 2 x 300 Mbits/s 45 000 Km

Page 8: 06-01- Characterisation of high bandwith 0.8 um laser

page 8 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

� 0,8 µm laser technology well suited for : · data relay services inter-orbital link including GEO-LEO, GEO-UAV,

GEO-Ground : long distance with frequent re-acquisitions · Short distance cluster or formation flying satellites· Compatible with Silicon sensors (several thousand of pixels) for

Pointing, Acquisition & Tracking · Compatible with communication data rate up to 600 Mbit/s

� Several missions to be launched in the period 2010 to 2015:· Military or European relay satellites: < 400 Mbps

· Cluster of co localised GEO satellites < 600 Mbps· Formation flying satellites (scientific, observation) < 100 Mbps

� Need for high power monomode laser diode source with bandwidth up to 600 Mbps.

3. Future applications of 0,8 µm optical link

Page 9: 06-01- Characterisation of high bandwith 0.8 um laser

page 9 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

4. Need for European laser diode manufacturer

� SILEX and OICETS communication laser diode : · SILEX :

� SDL 5411 G1 & 5421 G1(JDSU)

� Operating conditions: 120 mW p-p, OOK, 50 Mbps

· LUCE (OICETS) : � SDL 5430 G1

� Operating conditions: 200 mW p-p, OOK , 50 Mbps

� Current in orbit laser diodes are submitted to ITAR restrictions� Technology available in Europe, requires space qualification:

· LOLA demonstrator laser diode :� LUMICS LU848M160, identified by Alcatel Alenia Space (responsible of

communication equipments, metrology and optical critical components procurement in the frame of LOLA)

� Operating conditions: 320 mW p-p, OOK, 50 Mbps

Page 10: 06-01- Characterisation of high bandwith 0.8 um laser

page 10 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

5. Today’s Lumics laser diode for LOLA demonstrator

� Quantum well high powerlaser diode� Mirror passivation with mono crystalline layer on facet (LUMICS patent)� LOLA laser module bandwidth < 100 Mbps, used at 50 Mbps� Ouput power : 160 mW average power ex-PM fiber� Lot qualification for LOLA program� Butterfly package 14 pins with PM fiber� Fiber Bragg Grating

View inside Lumics package(with the courtesy of Alcatel Alenia Space)

Page 11: 06-01- Characterisation of high bandwith 0.8 um laser

page 11 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

6. Lumics laser diode improvements to increasebandwidth

� Reliability improvements :· Reduction of optical power density at chip facet

� Bandwidth improvements :· Reduction of metallization (reduce package capacitance)

· Wire bonding diameter increase (reduce package inductance)· Coplanar transmission line for HF signal current · Reduction of chip length (reduce laser diode capacitance)

� Power improvement:· Optimisation of ridge waveguide structure to improve chip-fiber coupling

Page 12: 06-01- Characterisation of high bandwith 0.8 um laser

page 12 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

7. High bandwidth Lumics laser diode (LUM0808M100, SN#136451)

� PM fiber 14 pins butterfly package with TEC

� Reduced length: 1,76 mm� Reduced metallization� No FBG� CW 100 mW . Peak-Peak:

200 mW� Design wavelength: 808 nm� Specification: bandwidth >

600 Mbps

Page 13: 06-01- Characterisation of high bandwith 0.8 um laser

page 13 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

8. First characterisation results

Laser diode characterisation test bench� Custom specific high frequency & high power laser driver LDD1-1T-CS developed by Alphalas:

· 1 GHz bandwidth· up to 400 mA DC current and +/-350 mA modulation current

� Laser diode module on butterfly laser mount� Modulation through external bias Tee (AC coupling)

Page 14: 06-01- Characterisation of high bandwith 0.8 um laser

page 14 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

First characterisation results on SN#136451

� L(I) measurements

Good correlation between measured and Lumics data sheet P(I)

� Optical spectrum measurement

Delta of 1.9 nm between measured and Lumics data sheet central wavelength under investigation

Lumics SN#136451

00,10,20,30,40,50,60,70,80,9

1

800 802 804 806 808 810 812 814 816 818 820

lambda (nm)

P (

norm

alis

ed)

P(I) Lumics SN#136451 @25°C

0

20

40

60

80

100

120

140

0 50 100 150 200 250

I (mA)

P (

mW

)

Measured Lumics data sheet

Page 15: 06-01- Characterisation of high bandwith 0.8 um laser

page 15 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

First characterisation results on SN#136451

� Transmit eye diagram with “1010” input signal at 311 Mbps

· Rise time & fall time < 900 ps· Jitter rms < 100 ps· Small infringement of transmit

mask

� Transmit eye diagram with “1010” input signal at 400 Mbps

· Rise time & fall time < 750 ps· Jitter rms < 75 ps· No infringement of transmit

mask

Page 16: 06-01- Characterisation of high bandwith 0.8 um laser

page 16 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

First characterisation results on SN#136451

� Transmit eye diagram with “1010”input signal at 500 Mbps

· Rise time & fall time < 560 ps· Jitter rms < 60 ps· Small infringement of transmit

mask & pulse shape distortion

� Receive eye diagram with PN7 input signal at 155 Mbps

· Receiver with STM1 data filter· Transmitter baseline wandering

effect enlarged the eye traces· Eye opening acceptable

Page 17: 06-01- Characterisation of high bandwith 0.8 um laser

page 17 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

First characterisation results on SN#136451

� Receive eye diagram with PN15 input signal at 622 Mbps

· Transmitter baseline wandering effect enlarged the eye traces

· Receiver with STM4 data filter· Eye diagram starts to close

Page 18: 06-01- Characterisation of high bandwith 0.8 um laser

page 18 WORKSHOP Laser diodes in Space – CNES – 11&12 mai 2006

9. Conclusion

� Promising preliminary results :· Technology compatible with 500 Mbps data rate (demonstrated

with test bench limitation, bandwidth limit of laser diode in the same order)

· Optical spectrum bandwidth < 1 nm

� Next activities:· Improvement of test bench metrology : more integrated coupling of

HF laser driver with laser diode· Characterisation of all diode items

� Future activities:· Increase of power of high bandwidth laser diode above 200 mW· Increase of bandwidth from 500 to 600 Mbps· Optimisation of coupling with FBG (for wavelength stabilisation)· Space qualification of laser module