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19/01/17 1 YFR8010 Practical Spectroscopy Jüri Krustok Lembit Kurik Urmas Nagel (KBFI) 1 YFR8010 Practical Spectroscopy I 4 laboratory works: 1. Raman spectroscopy 2. Photoluminescence 3. μ-Photoluminescence 4. External quantum efficiency of solar cell 2

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19/01/17

1

YFR8010 Practical Spectroscopy

Jüri Krustok Lembit Kurik

Urmas Nagel (KBFI)

1

YFR8010 Practical Spectroscopy I 4 laboratory works:

1.  Raman spectroscopy 2.  Photoluminescence 3.  µ-Photoluminescence 4.  External quantum efficiency of solar cell

2

19/01/17

2

YFR8010 Practical Spectroscopy Raman spectroscopy

Professor Jüri Krustok [email protected]

http://staff.ttu.ee/~krustok

3

History n Discovered in 1928: India (Raman, Krishnan)

and Soviet Union (Landsberg, Mandelstam) n  In 1928 Raman and Krishnan published a

paper in "Nature", but the explanation of the experiment was not correct.

n Few month later in 1928 Landsberg and Mandelstam published a paper with correct explanation.

n  In Soviet Union this effect was called combination scattering. 4

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3

Raman

5

Light and matter n  If the light is directed on to matter we observe

absorption, reflection and scattering. n  SCATTERING can be:

n  Elastic (Rayleigh) → λsecondary = λprimary

n  Nonelastic (Raman) → λsecondary ≠ λprimary

§  The wavelength of light changes with RAMAN scattering

6

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4

Elastic (Rayleigh) scattering

Intensity of scattering depends on the wavelength λ of primary light and on the scattering angle Θ Blue light is scattered more than red light Blue sky- Reyleigh scattering of sunlight on molecules of air! 7

Raman vs. Rayleigh scattering Raman scattering intensity is 107 times weaker than the primary light (laser) intensity

8

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5

Raman and FTIR (infrared spectroscopy) FTIR Raman

i. vibrational modes vibrational modes ii. change of dipole movement change in polarizability iii. Excitation of the molecule Light as an

electromagnetic field:

to higher vibrational electron state disturbing of electron cloud near the bond

δ- 2δ+ δ-

9

Physics of Raman effect n Raman spectra show very weak peaks with

frequency ω and this frequency is a combination of primary light frequency ω0 and the frequency of vibrational states of molecules (or vibrational modes of crystals) ωi.

iωωω ±= 010

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6

Laser photon is absorbed

Excited electron levels

A

A

Virtual levels

Raman theory

11

Rayleigh scattering energy does not change!! hνin = hνout

A Raman scattering energy changes!! hνin <> hνout

Raman theory

12

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7

Anti-Stokes: E = hν + ΔE

Stokes: E = hν - ΔE

Raman theory

ΔE is related to the vibrational states of the molecule

13

Raman spectroscopy: wavenumbers

λ(µm))(cmν410~ 1 =−

1 cm-1 = 0.12397 meV λ

ν1~ =

In spectra it means an energetic distance from laser line!!

14

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8

Raman spectrum In typical Raman spektrum we have: 1. Rayleigh peak (ΔE=0) 2. Anti-Stokes peaks, where the energy is increased, i.e. ΔE<0 3. Stokesi peaks, where the energy is decreased, i.e. ΔE>0 In general we record Stokesi peaks

15

Molecules and crystals

n Molecules – vibrations of molecules n Crystals- Lattice vibration modes (phonons) n  Lattice vibration modes depend on symmetry

of the lattice, atomic masses and bond strengths between atoms

16

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9

Example- chalcopyrite

CuInSe2 CuInS2 CuGaSe2 and others

17

Vibrational modes in chalcopyrite n  In chalcopyrite AIBIIIC2

VI crystal we have 8 atoms in unit cell. Accordingly we have 24 vibrational modes: 1A1 + 2A2 + 3B1 + 4B2 + 7E,

From them we have 22 Raman active modes: 1A1 + 3B1 + 3B2(LO) + 3B2(TO) + 6E(LO) + 6E(TO).

n  A1 always dominates spectra, because it is related to

anion movement only n  B1 mode is related to cation movement and B2 and E

modes are related to movement of all atoms. 18

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10

A1 mode in chalcopyrite

The most intensive peak in Raman spectra

19

A1 peaks in chalcopyrites

20

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11

Raman spectra of CuInS(Se)2

21

The shape of Raman peaks

Gauss shape

Lorenz shape

22

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12

Raman spectra Ramani peaks are very

close to the laser line n  The separation of peaks

is better with red laser n  Intensity of Raman

peaks is proportional to [1/λlaser]4

n  blue laser gives better signal!

400 Wavelength

0 10 20 30 40 50 60

Inte

nsity

B

LUE

lase

r

GR

N la

ser

RE

D

lase

r

Fluorescence

Raman shift

Fluorescence kills a weak Raman signal 23

Micro-Raman spectrometer

Laser

CCD Detector

Sample

Obj Lens

Notch Filter

24

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Notch filter

It is used to remove scattered laser light

25

Long-wave-pass filter

26

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Confocal microRaman

27

Raman spectrometer

HORIBA Jobin Yvon LabRam HR VI-143 room

28

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Raman spectrometer (from behind)

29

Scanning Raman

Micro scan from the surface of unknown pill 4 different peaks- 4 different colors

30

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Diamond Raman

1331.5 cm-1

Zirconia (used to replace diamond) :

31

Raman of different polymers

32

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Raman of human body

33

Raman of explosives

34

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18

Fitting of Raman (and PL) spectra n Free FITYK software http://www.unipress.waw.pl/fityk/

35

Raman measurements n Measure different samples n Spectra fitting with Lorenzian function n Find Imax, Emax, W for each peak

n Memory stick !!!!

36

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19

YFR8010 Practical Spectroscopy PHOTOLUMINESCENCE

Prof. Jüri Krustok

37

Photoluminescence in semiconductors

38

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20

Recombination

n Radiative recombination- photoluminescence

n Non radiative recombination- DARK!

39

Equipment for photoluminescence

40

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PL setup laser

41

PL measurements

Detectors: Photomultiplier tubes (PMT) :

FEU-79 (visible range)

R632- red and near infrared range

Semiconductor detectors:

Si- Visible and near infrared range (~1000nm)

InGaAs- near infrared range (~1700 nm)

PbS- infrared (~3000 nm) 42

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22

PL measurement software in TUT- LabView project

43

E, eV

Eg Band-to-band

Excitons Shallow defects

Deep defects

PL bands in semiconductors:

44

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23

Photoluminescence in semiconductors

n Recombination luminescence

n Center luminescence 45

Edge emission

46

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24

Edge emission

47

GaAs edge emission

)exp()(~)( 2/1

kTEh

EhAhI gg

−−−

ννν

48

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25

Edge emission is used in: n  LED (Light emitting diode) n Semiconductor lasers

49

Excitons

E (eV) Eg

FE

DX

AX

~meV

Exciton: electron and hole pair 50

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26

PL of excitons

S.H. Song et al. / Journal of Crystal Growth 257 (2003) 231–236

CdTe excitons

51

Excitons in CuInS2

52

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27

Photoluminescence of donor-acceptor pairs

53

Photoluminescence of donor-acceptor pairs

n  Probability of electron (on the donor defect) and hole (on the acceptor defect) recombination: WDA=Wo exp(-2R/ao)

n  The PL energy of each DA pair depends on the distance between donor and acceptor R:

n  In case of shallow levels we have a distribution of pairs:

ReEEERh ADgDA ε

ν2

)()( ++−=

)34exp(4)( 34 RNRNNRN DADDAπ

π −=54

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Photoluminescence of donor-acceptor pairs

classic work! DAP in GaP Phys. Rev. 133, 1964, p. A269

55

Photoluminescence of donor-acceptor pairs

DAP in GaP 56

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29

t-shift GaN MRS Internet J. Nitride Semicond. Res. 6, 12(2001).

Photoluminescence of donor-acceptor pairs

R increases W decreases t increases Emax decreases Closest pairs will recombine FASTER 57

j-shift Phys. Rev. B, 6, 1972, 3072

Photoluminescence of donor-acceptor pairs

R increases W decreases Ilaser increases Emax increases The recombination of DA pairs having larger distance will start to saturate, because the recombination probability W is small

58

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Deep donor-deep acceptor pairs -> DD-DA pairs.

n  DD-DA can be found in different materials. n  Only closest pairs can excist between these deep

defects, because of overlap of wave-functions. n  It is possible to find an energy difference between

closest pairs:

⎟⎟⎠

⎞⎜⎜⎝

⎛−=Δ

nmmn rr

eE 112

ε59

DD-DA pairs

D1 D2 W

ED0

EA0

c-band

v-band

as grown compensated

D1

D2

r1r2

r∞

60

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31

0.6 0.8 1.0 1.2

D6D1

CuInS2

E (eV)

D6 D1AgInS2

PL i

nten

sity (

a.u.)

D6 D1

CuGaSe2

D6

D1

CuIn0.5

Ga0.5

Se2

DD-DA pairs in different ternaries. Theoretical positions are marked with vertical lines

DD-DA pairs

61

0.50 0.55 0.60 0.650

1

2

3

4

5

hω1

hω2

T=8K

CuInS2

a)

PL in

tens

ity (a

. u.)

E (eV)

0.620 0.625 0.630

D50

D40

b)

DD-DA pairs can also bound excitons: Deep excitons in CuInS2.

DD-DA pairs

62

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DD-DA pairs in CdTe

Different interstitial positions- different PL bands

J. Krustok, H. Collan, K. Hjelt, J. Mädasson, V. Valdna. J.Luminescence , v. 72-74, pp. 103-105 (1997).

63

0.8 1.0 1.20

1

2

3

4

5

c-AgInS2

T=8K

D6

D5D4

D3 D2D1

PL in

tens

ity (a

. u.)

E (eV)

0.6 0.8 1.0 1.20

20

40T=8K

o-AgInS2

D6 D4D5 D3 D2 D1

PL in

tens

ity (a

. u.)

E (eV)

0.0

0.1

0.2

0.3

0.4

0.5

0.6

DD-DA pairs in AgInS2

Chalcopyrite Orthorombic

64

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33

ET

PL

Thermally liberated holes

Temperature quenching of PL

0 20 40 60 80 100 120 140-5

-4

-3

-2

-1

0

1

2

Fitting Experiment

ln (I)

1000/T (1/K)

ET =114 ± 6 meV

65

Temperature quenching of PL

q THEORY:

q J. Krustok, H. Collan, and K. Hjelt. J. Appl. Phys. v. 81, N 3, pp. 1442-1445 (1997) .

( )( )kTETT

ITIT /exp1 2

3

223

1

0

−++=

ϕϕ

66

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34

Shape of PL band

n  Theory – Pekar, Huang, Rhys, jt. n  The shape is not easy to calculate n  Simplifications:

n  T=0 n  only one phonon is present and not the phonon

spectrum

Then in is possible to find transition probability from each energy level of excited state to each energy level of ground state- all these probabilities follow Poisson distribution

67

Poisson distribution !)exp()(

rrP

r µµ −=

68

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35

Shape of PL band

n  The theoretical shape of PL band is:

∑ −−−

=m

m

EmEmSSIEI )(

!)exp()( 00 ωδ !

The shape of each m-th small PL band depends mainly on interactions with acoustic phonons

69

Shape of PL band

0.00

10.00

20.00

30.00

40.00

50.00

60.00

70.00

80.00

90.00

100.00

0.85 0.90 0.95 1.00 1.05

IntF(x)

∑ −−−

=m

m

EmEmSSIEI )(

!)exp()( 00 ωδ !

E0 m=0

m=1

m=2

phonon energy

Phonon replicas having Gaussian shape

0-phonon peak

PEKARIAN

S=0.47

70

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36

0.50 0.55 0.60 0.650

1

2

3

4

5

hω1

hω2

T=8K

CuInS2

a)

PL in

tensit

y (a.

u.)

E (eV)

0.620 0.625 0.630

D50

D40

b)

Shape of PL band

PL band in CuInS2

two phonons can be seen

71

Shape of PL band

( )⎥⎦

⎤⎢⎣

⎡ −−= 2

2max

02ln4exp)(WEEIEI

Gaussian shape:

( )⎥⎦

⎤⎢⎣

⎡ −−−= 2

20

0 )(2ln82ln4exp)(

ωω

!!

SSEEIEI

If in Pekarian S -> ∞, then we also will have a pure Gaussian shape:

72

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37

0.80 0.85 0.90 0.95 1.00 1.050

50000

100000

150000

200000

PL in

tens

ity (a

. u.)

E (eV)

0

5000

10000

15000

20000

Shape of PL band

Lorenz shape

Gaussian shape

73

PL of heavily “doped” semiconductors

n  Most of ternaries and quaternary compounds are heavily doped, i.e. they have hudge amount of defects.

n  distance between defects is smaller than the Bohr radius of electrons and holes on defects-> heavy doping.

n  Edges of conduction and valence bands are curved because of potential fluctuations.

74

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38

1.05 1.10 1.15 1.20 1.25 1.30

0.0

0.2

0.4

0.6

0.8

1.0T=12.5K

PL in

tensit

y

E, eV

• J. Krustok, H. Collan, M.Yakushev, K. Hjelt. Therole of spatial potentialfluctuations in the shape ofthe PL bands of multinarysemiconductor compounds.Physica Scripta , T79, pp.179-182 (1999).

PL of heavily “doped” semiconductors

Typical PL spectrum in CuInGaSe2

75

Theory of heavily doped materials

Fn

Eg

ε

BBBT

ρc

ρv

Ec

Ev

Theory: Shklovskii, Efros Levaniuk, Osipov

76

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39

1.1 1.2 1.3 1.40

1

2

3

4

5

240 K210 K

190 K175 K160 K145 K130 K120 K110 K95 K

80 K70 K60 K50 K40 K30 K20 K15 K12.5 K

PL in

tensit

y (a.

u.)

E (eV )

BB-band

BT-band

• J. Krustok, H. Collan, M.Yakushev, K. Hjelt. Therole of spatial potentialfluctuations in the shape ofthe PL bands of multinarysemiconductor compounds.Physica Scripta , T79, pp.179-182 (1999).

Edge emission of CuInGaSe2

BB and BT bands

77

Temperature dependence of BB and BT bands

0 50 100 150 200 2501.21

1.22

1.23

1.24

1.29

1.30

1.31

T2 = 175K

hνmax~ 2.1kT

BT- band

BB- band

T1=96K

hνmax~ - 4.4kT

hνm

ax (

eV)

T (K)

• J. Krustok, J. Raudoja, M.Yakushev, R. D.Pilkington, and H. Collan.phys. stat. sol. (a) v. 173,No 2, pp. 483-490 (1999).• J. Krustok, H. Collan, M.Yakushev, K. Hjelt.Physica Scripta , T79,pp. 179-182 (1999).

78

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PL of heavily “doped” semiconductors

79

PL measurements n Measure PL spectra n Spectra fitting with Gaussian function n Find Imax, Emax and W for each PL band

80

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41

YFR8010 Practical Spectroscopy Spectral Response of Solar Cells

Professor Jüri Krustok [email protected]

http://staff.ttu.ee/~krustok

81

I-V Curve of Solar Cell

82

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42

Spectral Response

ideal solar cell

Lost current

83

Spectral Response- theory

2. Experimental

CZTSmonograinswere synthesized from binaries and elemental S inmolten flux by isothermal recrystallization process. The details of themonograin growth technology can be found elsewhere [18]. MGL solarcells with structure: graphite/MGL/CdS/ZnO/glass, were made frompowder crystals with a diameter of 56–63 μm as selected by sieving.The analysis area of the solar cell is determined by the back contactarea which is typically about 0.04 cm2. More details about the solarcell preparation can be found in [19].

For the temperature dependent J–V and EQE measurements solarcells were mounted in a closed cycle He cryostat. J–V measurementswere done by decreasing the temperature while EQE measurementswere done by increasing the temperature in the range T = 10–300 K.For EQE measurements the generated photocurrent was detected at0 V bias voltage. 250W standard halogen lampwith calibrated intensity(100 mW cm−2) was used as a light source and spectrally neutral netfilters for intensity dependence.

3. Results and discussion

Room temperature J–V characteristics of a studied CZTS-based MGLsolar cell showed the following properties: open-circuit voltage Voc =709 mV, short-circuit current density Jsc = 13.8 mA/cm2, fill factorFF = 61.4%, and efficiency η = 6.0%. Due to the peculiarity of the MGLsolar cell structure, the active area where the photocurrent is actuallyproduced is smaller than the analysis area. The active area is estimatedto be 75% of the back contact area after excluding the area of the bindermaterial between the absorber material powder crystals. After suchconsideration the current density per absorber material active area isestimated to be Jscabs. = 18.4 mA/cm2 and the efficiency is estimated tobe ηabs = 8.0%. In spite of that, solar cell parameters are still limiteddue to recombination and parasitic losses. The series resistances obtain-ed from the light and the dark J–V curves determined at room temper-ature by the process described by Hegedus and Shafarman [20] arerather high, Rslight = 3.6 Ω cm2 and Rsdark = 4.5 Ω cm2, accordingly.

The thermal behavior of the Voc under different light intensities isshown in Fig. 1. It is known [21] that the temperature dependence ofVoc near room temperature can be presented as

VOC ¼ EAq−nkT

qln

I00IL

! "; ð1Þ

where EA, n, k, I00, and IL are the activation energy, diode ideality factor,Boltzmann constant, reverse saturation current prefactor, and the pho-tocurrent, respectively. In general, the activation energy EA and also I00depend mainly on the dominating recombination mechanism in the

solar cell. In case of bulk recombination EA≈ Eg, where Eg is the bandgapenergy of the absorber material. The bandgap energy of CZTS slightlydepends on the type of crystal structure [12], but is usually higherthan 1.5 eV. In our sample EA ≈ 1.26 eV was determined from the Voc

(T) plot (see Fig. 1). In general, according to the theory [22] in case ofEA b Eg, the interface recombination is a dominating recombination.

The temperature dependence of the series resistance Rs found usingFig. 2 is shown in Fig. 3a where three different regions can be distin-guished. At temperatures T N 90 K (region I) Rs decreases with increas-ing temperature indicating the thermal activation of carriers [23]. Inthis region, the Rs can be presented as:

RS ¼ RS0 exp EA=kTð Þ ð2Þ

where the exponential prefactor RS0 contains all parameters that are in-dependent or weekly dependent on temperature. Using Eq. (2) the acti-vation energies EA, d=87± 3meV and EA, l=43± 1meV for dark andlight curves were found, respectively. These activation energies are inthe same range as found in [6,8,24]. At intermediate temperatures(T=90–40K, region II), the dependence of the series resistance on tem-perature changes and a typical Mott's variable-range hopping (VRH)conduction starts to dominate [25]. This type of behavior is expectedin all heavily dopedmaterialswhere spatial potentialfluctuations createdeep potential wells for holes [6,26,27]. At the same time, we also ex-pect the increasing role of bulk recombination in this temperature re-gion and therefore the VRH model is not completely valid here. Atabout T=40 K, a rapid change of Rs can be seen. In low temperature re-gion (T b 40 K, region III), Rs drops downmore than one order of magni-tude and remains almost constant down to the lowest measuredtemperature. At these very low temperatures, generated holes are notable to tunnel through the potential barrier into the interface region be-tween CZTS and CdS and therefore the interface recombination ratemust be very low.

Quantum efficiency measurement is a well-known method to de-scribe optical and electronic losses in solar cell devices. From the low-energy side of the EQE curve i.e. near the bandgap energy E≈ Eg, the ef-fective bandgap energy Eg⁎ can be determined [17] by using an approx-imation proposed by Klenk and Schock [28]:

EQE≈ KαLeff ≈ A E−E$g# $1=2

=E ð3Þ

where constant A includes all energy independent parameters,Leff = w + Ld is the effective diffusion length of minority carriers,Ld is their diffusion length in the absorber material, w is the widthof the depletion region, and α is the absorption coefficient of the ab-sorber material. The constant K is unity in absolute measurements.Consequently, the Eg⁎ value can be determined from a plot of

Fig. 1. Temperature dependence of Voc measured at different light intensities. Fig. 2. Temperature dependence of dark J–V curves.

163M. Danilson et al. / Thin Solid Films 582 (2015) 162–165

EXTERNAL QUANTUM EFFICIENCY

84

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43

Fiding Eg

85

Finding Eg

2. Experimental

CZTSmonograinswere synthesized from binaries and elemental S inmolten flux by isothermal recrystallization process. The details of themonograin growth technology can be found elsewhere [18]. MGL solarcells with structure: graphite/MGL/CdS/ZnO/glass, were made frompowder crystals with a diameter of 56–63 μm as selected by sieving.The analysis area of the solar cell is determined by the back contactarea which is typically about 0.04 cm2. More details about the solarcell preparation can be found in [19].

For the temperature dependent J–V and EQE measurements solarcells were mounted in a closed cycle He cryostat. J–V measurementswere done by decreasing the temperature while EQE measurementswere done by increasing the temperature in the range T = 10–300 K.For EQE measurements the generated photocurrent was detected at0 V bias voltage. 250W standard halogen lampwith calibrated intensity(100 mW cm−2) was used as a light source and spectrally neutral netfilters for intensity dependence.

3. Results and discussion

Room temperature J–V characteristics of a studied CZTS-based MGLsolar cell showed the following properties: open-circuit voltage Voc =709 mV, short-circuit current density Jsc = 13.8 mA/cm2, fill factorFF = 61.4%, and efficiency η = 6.0%. Due to the peculiarity of the MGLsolar cell structure, the active area where the photocurrent is actuallyproduced is smaller than the analysis area. The active area is estimatedto be 75% of the back contact area after excluding the area of the bindermaterial between the absorber material powder crystals. After suchconsideration the current density per absorber material active area isestimated to be Jscabs. = 18.4 mA/cm2 and the efficiency is estimated tobe ηabs = 8.0%. In spite of that, solar cell parameters are still limiteddue to recombination and parasitic losses. The series resistances obtain-ed from the light and the dark J–V curves determined at room temper-ature by the process described by Hegedus and Shafarman [20] arerather high, Rslight = 3.6 Ω cm2 and Rsdark = 4.5 Ω cm2, accordingly.

The thermal behavior of the Voc under different light intensities isshown in Fig. 1. It is known [21] that the temperature dependence ofVoc near room temperature can be presented as

VOC ¼ EAq−nkT

qln

I00IL

! "; ð1Þ

where EA, n, k, I00, and IL are the activation energy, diode ideality factor,Boltzmann constant, reverse saturation current prefactor, and the pho-tocurrent, respectively. In general, the activation energy EA and also I00depend mainly on the dominating recombination mechanism in the

solar cell. In case of bulk recombination EA≈ Eg, where Eg is the bandgapenergy of the absorber material. The bandgap energy of CZTS slightlydepends on the type of crystal structure [12], but is usually higherthan 1.5 eV. In our sample EA ≈ 1.26 eV was determined from the Voc

(T) plot (see Fig. 1). In general, according to the theory [22] in case ofEA b Eg, the interface recombination is a dominating recombination.

The temperature dependence of the series resistance Rs found usingFig. 2 is shown in Fig. 3a where three different regions can be distin-guished. At temperatures T N 90 K (region I) Rs decreases with increas-ing temperature indicating the thermal activation of carriers [23]. Inthis region, the Rs can be presented as:

RS ¼ RS0 exp EA=kTð Þ ð2Þ

where the exponential prefactor RS0 contains all parameters that are in-dependent or weekly dependent on temperature. Using Eq. (2) the acti-vation energies EA, d=87± 3meV and EA, l=43± 1meV for dark andlight curves were found, respectively. These activation energies are inthe same range as found in [6,8,24]. At intermediate temperatures(T=90–40K, region II), the dependence of the series resistance on tem-perature changes and a typical Mott's variable-range hopping (VRH)conduction starts to dominate [25]. This type of behavior is expectedin all heavily dopedmaterialswhere spatial potentialfluctuations createdeep potential wells for holes [6,26,27]. At the same time, we also ex-pect the increasing role of bulk recombination in this temperature re-gion and therefore the VRH model is not completely valid here. Atabout T=40 K, a rapid change of Rs can be seen. In low temperature re-gion (T b 40 K, region III), Rs drops downmore than one order of magni-tude and remains almost constant down to the lowest measuredtemperature. At these very low temperatures, generated holes are notable to tunnel through the potential barrier into the interface region be-tween CZTS and CdS and therefore the interface recombination ratemust be very low.

Quantum efficiency measurement is a well-known method to de-scribe optical and electronic losses in solar cell devices. From the low-energy side of the EQE curve i.e. near the bandgap energy E≈ Eg, the ef-fective bandgap energy Eg⁎ can be determined [17] by using an approx-imation proposed by Klenk and Schock [28]:

EQE≈ KαLeff ≈ A E−E$g# $1=2

=E ð3Þ

where constant A includes all energy independent parameters,Leff = w + Ld is the effective diffusion length of minority carriers,Ld is their diffusion length in the absorber material, w is the widthof the depletion region, and α is the absorption coefficient of the ab-sorber material. The constant K is unity in absolute measurements.Consequently, the Eg⁎ value can be determined from a plot of

Fig. 1. Temperature dependence of Voc measured at different light intensities. Fig. 2. Temperature dependence of dark J–V curves.

163M. Danilson et al. / Thin Solid Films 582 (2015) 162–165

86

19/01/17

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Finding Eg

1,25 1,30 1,35 1,40 1,45 1,50 1,55 1,600,0

0,3

0,6

0,9

1,2

1,5

1,8

2,1

2,4

2,7

(hν*

EQE)

2 (arb

.unit

s)

E(eV)

SnST=300K

Eg=(1,298±0,005) eV

Eg=(1,411±0,008) eV

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What to do? n Measure EQE (E) spectrum for solar cell n Draw (EQE*E)2 vs E curves

n Calculate Eg

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19/01/17

45

Meeting point U06 first floor end of the building room 156 Phone: +372 5236945

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