Details
Originalsprache | Englisch |
---|---|
Titel des Sammelwerks | 2023 13th European Space Power Conference, ESPC 2023 |
Herausgeber (Verlag) | Institute of Electrical and Electronics Engineers Inc. |
ISBN (elektronisch) | 9798350328998 |
ISBN (Print) | 979-8-3503-2900-1 |
Publikationsstatus | Veröffentlicht - 2023 |
Veranstaltung | 13th European Space Power Conference, ESPC 2023 - Elche, Spanien Dauer: 2 Okt. 2023 → 6 Okt. 2023 |
Abstract
New technology trends in space, such as the use of GaN FETs in power applications, increase the need for a PWM controller IC that can directly drive GaN FETs while being reliable and easy to use. In this paper, the radiation performance of a newly developed prototype radiation-resistant PWM controller IC for a wide power range and new technology applications in space is presented. To ensure reliability in the space environment, this prototype IC was tested for total ionizing dose and destructive single event effects. This paper analyzes the test results and identifies possible improvements to the circuit or application. A maximum total ionizing dose of 185 krad was achieved. Some variations in parameters were observed during the test. The DSEE test was performed with Xe ions to test the DSEE's disruptive strength. The DSEE test shows no destructive events for the tested conditions such as a power bus voltage of 105 V. With this information, this paper paves the way for design change and further testing in the future to obtain evaluation results according to the ESCC.
ASJC Scopus Sachgebiete
- Energie (insg.)
- Energieanlagenbau und Kraftwerkstechnik
- Ingenieurwesen (insg.)
- Elektrotechnik und Elektronik
- Ingenieurwesen (insg.)
- Luft- und Raumfahrttechnik
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2023 13th European Space Power Conference, ESPC 2023. Institute of Electrical and Electronics Engineers Inc., 2023.
Publikation: Beitrag in Buch/Bericht/Sammelwerk/Konferenzband › Aufsatz in Konferenzband › Forschung › Peer-Review
}
TY - GEN
T1 - TID and DSEE Effects in a GaN FET Capable PWM Controller IC Prototype for Space Applications
AU - Mand, Philipp
AU - Burkhay, Volodymyr
AU - Rocke, Andre
AU - Gieselmann, Uwe
AU - Fauth, Leon
AU - Olbrich, Markus
AU - Oliver, Jesus
AU - Wicht, Bernhard
AU - Friebe, Jens
N1 - Publisher Copyright: © 2023 IEEE.
PY - 2023
Y1 - 2023
N2 - New technology trends in space, such as the use of GaN FETs in power applications, increase the need for a PWM controller IC that can directly drive GaN FETs while being reliable and easy to use. In this paper, the radiation performance of a newly developed prototype radiation-resistant PWM controller IC for a wide power range and new technology applications in space is presented. To ensure reliability in the space environment, this prototype IC was tested for total ionizing dose and destructive single event effects. This paper analyzes the test results and identifies possible improvements to the circuit or application. A maximum total ionizing dose of 185 krad was achieved. Some variations in parameters were observed during the test. The DSEE test was performed with Xe ions to test the DSEE's disruptive strength. The DSEE test shows no destructive events for the tested conditions such as a power bus voltage of 105 V. With this information, this paper paves the way for design change and further testing in the future to obtain evaluation results according to the ESCC.
AB - New technology trends in space, such as the use of GaN FETs in power applications, increase the need for a PWM controller IC that can directly drive GaN FETs while being reliable and easy to use. In this paper, the radiation performance of a newly developed prototype radiation-resistant PWM controller IC for a wide power range and new technology applications in space is presented. To ensure reliability in the space environment, this prototype IC was tested for total ionizing dose and destructive single event effects. This paper analyzes the test results and identifies possible improvements to the circuit or application. A maximum total ionizing dose of 185 krad was achieved. Some variations in parameters were observed during the test. The DSEE test was performed with Xe ions to test the DSEE's disruptive strength. The DSEE test shows no destructive events for the tested conditions such as a power bus voltage of 105 V. With this information, this paper paves the way for design change and further testing in the future to obtain evaluation results according to the ESCC.
KW - Driver
KW - GaN
KW - Hi-Rel
KW - PWM
KW - rad-hard
KW - radiation
KW - SEE
KW - Single Event Effect
KW - Space
KW - TID
KW - Total Ionizing Dose
UR - http://www.scopus.com/inward/record.url?scp=85185004113&partnerID=8YFLogxK
U2 - 10.1109/espc59009.2023.10413257
DO - 10.1109/espc59009.2023.10413257
M3 - Conference contribution
AN - SCOPUS:85185004113
SN - 979-8-3503-2900-1
BT - 2023 13th European Space Power Conference, ESPC 2023
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 13th European Space Power Conference, ESPC 2023
Y2 - 2 October 2023 through 6 October 2023
ER -