Josef Blazej

Dr. Josef Blazej

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Research Focus & Metrics

Academic Career Length

30Years (1997-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 March 2011 in Metrologia
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Journal Article
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IPIvan Prochazka
Ivan Prochazka
JBJosef Blazej
Josef Blazej
JKJan Kodet
Jan Kodet

1 December 2012 in Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment
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Journal Article
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JKJan Kodet
Jan Kodet
IPIvan Prochazka
Ivan Prochazka
JBJosef Blazej
Josef Blazej
XSXiaoli Sun
Xiaoli Sun
JCJohn Cavanaugh
John Cavanaugh

1 April 2013 in Review of Scientific Instruments
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Journal Article
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IPIvan Prochazka
Ivan Prochazka
JKJan Kodet
Jan Kodet
JBJosef Blazej
Josef Blazej
We are reporting on a design, construction, and performance of photon counting detector packages based on solid state sensors. These photon counting devices have been optimized for extremely high stability of their detection delay. The detectors have been designed for applications in fundamental metrology and optical time transfer. The single photon avalanche diode structure manufactured on silicon using the K14 technology is used as a sensor. The active area of the sensor is circular with a diameter of 100 or 200 μm. The sensor is operated in an active quenching and gating mode. The photon detection efficiency exceeds 40% in a wavelength range spanning from 500 to 800 nm. The timing resolution is better than 20 ps rms. Its detection delay is stable within ±600 fs over several days of operation, in a sense of time deviation the detection delay stability of 150 fs has been achieved. The temperature change of the detection delay is as low as 280 fs/K. This timing performance is preserved even under extremely high background photon fluxes exceeding 100 Mc/s. The detectors have been qualified for operation in space missions.

1 August 2014 in Advances In Space Research
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Journal Article
Closed access
IPIvan Prochazka
Ivan Prochazka
JKJan Kodet
Jan Kodet
JBJosef Blazej
Josef Blazej
GKGeorg Kirchner
Georg Kirchner
FKFranz Koidl
Franz Koidl

22 December 1997
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Conference Paper
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GKGeorg Kirchner
Georg Kirchner
FKFranz Koidl
Franz Koidl
JBJosef Blazej
Josef Blazej
KHKarel Hamal
Karel Hamal
IPIvan Prochazka
Ivan Prochazka
The SPAD has proven already its capability of timing single- photon events with picosecond accuracy; it does that also for multi-photon events, but introduces here a time walk effect: with received energies of 1000 photons and more, the measured epoch time is shifted 200 ps or more towards earlier times; although the specific SPAD type used shows the lowest time walk effect of all measured silicon avalanche diodes, this effect still might introduce range errors of up to 30 mm, when measuring distances to satellites. It has been shown that this time walk effect is connected with a very small change of the avalanche rise time; this effect has been successfully used to develop an electronic circuit which measures this rise time difference, and uses it to compensate automatically almost all of the time walk effect. Some prototypes have been built and tested successfully in the satellite laser ranging station Graz; improved versions of the circuit are operated or tested now successfully in other SLR stations. It has been shown that the time walk effect can be reduced to more or less zero, for a dynamical range from single photon up to more than 1000 photons. For best time walk compensation, the circuit is adjusted for a specific laser pulse length; it has been shown however, that this adjustment also gives good time walk compensation for other laser pulse lengths.

1 May 2016 in Review of Scientific Instruments
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Journal Article
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IPIvan Prochazka
Ivan Prochazka
JKJan Kodet
Jan Kodet
JBJosef Blazej
Josef Blazej
The laser time transfer link is under construction for the European Space Agency in the frame of Atomic Clock Ensemble in Space. We have developed and tested the flying unit of the photon counting detector optimized for this space mission. The results are summarized in this Note. An extreme challenge was to build a detector package, which is rugged, small and which provides long term detection delay stability on picosecond level. The device passed successfully all the tests required for space missions on the low Earth orbits. The detector is extremely rugged and compact. Its long term detection delay stability is excellent, it is better than ±1 ps/day, in a sense of time deviation it is better than 0.5 ps for averaging times of 2000 s to several hours. The device is capable to operate in a temperature range of −55 °C up to +60 °C, the change of the detection delay with temperature is +0.5 ps/K. The device is ready for integration into the space structure now.