Research output: Contribution to journal › Conference article › peer-review
Calibration setup with metrological support for space qualified electric field probe. / Kozlov, Alexey; Shilov, Alexander; Styuf, Alexey et al.
In: MATEC Web of Conferences, Vol. 158, 19.03.2018.Research output: Contribution to journal › Conference article › peer-review
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TY - JOUR
T1 - Calibration setup with metrological support for space qualified electric field probe
AU - Kozlov, Alexey
AU - Shilov, Alexander
AU - Styuf, Alexey
AU - Doroshkin, Alexander
AU - Nikitenko, Anatoly
PY - 2018/3/19
Y1 - 2018/3/19
N2 - The article shows the results of calculations necessary for testing to approve the space qualified electric field probe used in outer space. A special electric field probe calibration setup was developed and manufactured, which allows testing a space qualified electric field probe in the entire measurement range (from ± 0.1 to ± 200 kV/m) under low (-80 °C) and high (+72 °C) temperatures and at reduced pressure of 1.3 · 10-3 Pa (10-5 torr). Metrological tests of the probes batch, calibrated by the space qualified electric field probe calibrator, performed at the verification equipment under normal conditions, showed that the maximum error of the electric field probe does not exceed 15% in the entire measurements range which will increase the accuracy of determining the satellite surface charging parameters and help in designing modern spacecrafts.
AB - The article shows the results of calculations necessary for testing to approve the space qualified electric field probe used in outer space. A special electric field probe calibration setup was developed and manufactured, which allows testing a space qualified electric field probe in the entire measurement range (from ± 0.1 to ± 200 kV/m) under low (-80 °C) and high (+72 °C) temperatures and at reduced pressure of 1.3 · 10-3 Pa (10-5 torr). Metrological tests of the probes batch, calibrated by the space qualified electric field probe calibrator, performed at the verification equipment under normal conditions, showed that the maximum error of the electric field probe does not exceed 15% in the entire measurements range which will increase the accuracy of determining the satellite surface charging parameters and help in designing modern spacecrafts.
UR - http://www.scopus.com/inward/record.url?scp=85047729555&partnerID=8YFLogxK
U2 - 10.1051/matecconf/201815801022
DO - 10.1051/matecconf/201815801022
M3 - Conference article
AN - SCOPUS:85047729555
VL - 158
JO - MATEC Web of Conferences
JF - MATEC Web of Conferences
SN - 2261-236X
T2 - 6th International Forum for Young Scientists on Space Engineering 2018
Y2 - 26 April 2018 through 28 April 2018
ER -
ID: 13668854