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V' Au, C' Charles, R' W' Boswell

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Title: V' Au, C' Charles, R' W' Boswell


1
Evolution of stress in plasma-deposited films
  • V. Au, C. Charles, R. W. Boswell
  • Space Plasma and Plasma Processing, Plasma
    Research Laboratory
  • Research School of Physical Sciences and
    Engineering, The Australian National University,
    Canberra ACT AUSTRALIA 0200

Stress-thickness relationship Ex-situ
post-deposition etch-back
ABSTRACT We have investigated the
stress-thickness relationship for single phase
and multiple layers of silicon dioxide films (up
to 1mm thickness) deposited by helicon activated
reactive evaporation, a plasma assisted
deposition with electron beam evaporation. The
stress-thickness behaviour in the initial 400nm
is found to be strongly influenced by the number
of film layers deposited by stop-start
deposition.
Single phase vs multiple layer deposition
In-situ stress-curvature measurement
  • We measure a deflection in the laser spot. Two
    considerations to the deflection measured
  • a) Increasing film thickness during deposition
  • b) Position of laser on the bowed film and
    substrate
  • Bowing due to stress plotted as a function of
    film thickness. The bowing was measured using a
    Tencor P-10 surface profiler.
  • A linear relationship of the form B mtc was
    determined for bowing vs film thickness.

Experimental deposition details
  • The helicon activated reactive evaporation
    system (HARE) is a low temperature (200?C), low
    pressure (10-6 Torr), high density plasma
    deposition system.
  • Solid source silicon is evaporated by the e-beam
    transported through an oxygen argon plasma
  • In-situ stress-curvature measurements can be
    performed, as shown below

Experiment
Model
  • Multiple layer deposition the distinct
    depositions of the 4x ATM PR sample are clearly
    shown.
  • Single phase deposition measurements taken at 5
    minute intervals indicate the deflection trend
    during a continuous deposition of approx. 30
    minutes. Deflection occurs in both cases when a
    deposition is stopped and most distinctly when
    the system is brought to atmospheric pressure.

CONCLUSIONS By employing both an ex-situ
post-deposition etch-back technique and an
in-situ stress deflection measurement method, we
have shown the stress within a single phase
continuous film deposition to differ remarkably
strongly from that of a multiple layer
stop-start deposition, despite comparatively
little variation in the final measured stress of
the total film thickness. The in-situ deflection
method appears to be a promising direct and
non-invasive technique for the measurement of
stress during deposition. Calibration of the
laser setup is being undertaken.
Experiment
  • Ex-situ stress study SiO2 films of 1mm total
    thickness were deposited a single phase
    continuous film of 1 layer x 1mm, and multiple
    layer depositions of 2 layers x 0.5mm, 4 layers x
    0.25mm and 8 layers x 0.125mm
  • E-beam plasma were OFF between layer
    depositions for 1.5 minutes.
  • In-situ stress-curvature study Deflection due to
    stress-induced curvature was measured during the
    depositions of a single phase 1mm thickness SiO2
    film and a multiple layer 4 x 0.25mm SiO2 film.
  • Deposition system was brought to atmospheric
    pressure (ATM PR) between layer depositions. One
    layer was deposited per day.

Model
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