Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66
Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drif...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Satpathy, Dibyesh [verfasserIn] |
|---|
| Format: |
E-Artikel |
|---|---|
| Sprache: |
Englisch |
| Erschienen: |
2023 |
|---|
| Schlagwörter: |
|---|
| Anmerkung: |
© The Author(s) 2023 |
|---|
| Übergeordnetes Werk: |
Enthalten in: Journal of electric propulsion - Cham : Springer International Publishing, 2022, 2(2023), 1 vom: 01. Feb. |
|---|---|
| Übergeordnetes Werk: |
volume:2 ; year:2023 ; number:1 ; day:01 ; month:02 |
| Links: |
|---|
| DOI / URN: |
10.1007/s44205-023-00037-y |
|---|
| Katalog-ID: |
SPR049215264 |
|---|
| LEADER | 01000caa a22002652 4500 | ||
|---|---|---|---|
| 001 | SPR049215264 | ||
| 003 | DE-627 | ||
| 005 | 20230510061903.0 | ||
| 007 | cr uuu---uuuuu | ||
| 008 | 230202s2023 xx |||||o 00| ||eng c | ||
| 024 | 7 | |a 10.1007/s44205-023-00037-y |2 doi | |
| 035 | |a (DE-627)SPR049215264 | ||
| 035 | |a (SPR)s44205-023-00037-y-e | ||
| 040 | |a DE-627 |b ger |c DE-627 |e rakwb | ||
| 041 | |a eng | ||
| 100 | 1 | |a Satpathy, Dibyesh |e verfasserin |4 aut | |
| 245 | 1 | 0 | |a Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| 264 | 1 | |c 2023 | |
| 336 | |a Text |b txt |2 rdacontent | ||
| 337 | |a Computermedien |b c |2 rdamedia | ||
| 338 | |a Online-Ressource |b cr |2 rdacarrier | ||
| 500 | |a © The Author(s) 2023 | ||
| 520 | |a Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. | ||
| 650 | 4 | |a Drift-free-thrust stand |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Hall thruster |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Neutral flow |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Thruster with anode layer |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Kawabata, Shu |4 aut | |
| 700 | 1 | |a Sekine, Hokuto |4 aut | |
| 700 | 1 | |a Kawashima, Rei |4 aut | |
| 700 | 1 | |a Komurasaki, Kimiya |4 aut | |
| 700 | 1 | |a Koizumi, Hiroyuki |4 aut | |
| 773 | 0 | 8 | |i Enthalten in |t Journal of electric propulsion |d Cham : Springer International Publishing, 2022 |g 2(2023), 1 vom: 01. Feb. |w (DE-627)1770075232 |w (DE-600)3092981-7 |x 2731-4596 |7 nnns |
| 773 | 1 | 8 | |g volume:2 |g year:2023 |g number:1 |g day:01 |g month:02 |
| 856 | 4 | 0 | |u https://dx.doi.org/10.1007/s44205-023-00037-y |z kostenfrei |3 Volltext |
| 912 | |a GBV_USEFLAG_A | ||
| 912 | |a SYSFLAG_A | ||
| 912 | |a GBV_SPRINGER | ||
| 912 | |a GBV_ILN_11 | ||
| 912 | |a GBV_ILN_20 | ||
| 912 | |a GBV_ILN_22 | ||
| 912 | |a GBV_ILN_23 | ||
| 912 | |a GBV_ILN_24 | ||
| 912 | |a GBV_ILN_31 | ||
| 912 | |a GBV_ILN_39 | ||
| 912 | |a GBV_ILN_40 | ||
| 912 | |a GBV_ILN_60 | ||
| 912 | |a GBV_ILN_62 | ||
| 912 | |a GBV_ILN_63 | ||
| 912 | |a GBV_ILN_65 | ||
| 912 | |a GBV_ILN_69 | ||
| 912 | |a GBV_ILN_70 | ||
| 912 | |a GBV_ILN_73 | ||
| 912 | |a GBV_ILN_95 | ||
| 912 | |a GBV_ILN_105 | ||
| 912 | |a GBV_ILN_110 | ||
| 912 | |a GBV_ILN_151 | ||
| 912 | |a GBV_ILN_161 | ||
| 912 | |a GBV_ILN_170 | ||
| 912 | |a GBV_ILN_213 | ||
| 912 | |a GBV_ILN_230 | ||
| 912 | |a GBV_ILN_285 | ||
| 912 | |a GBV_ILN_293 | ||
| 912 | |a GBV_ILN_370 | ||
| 912 | |a GBV_ILN_602 | ||
| 912 | |a GBV_ILN_2014 | ||
| 912 | |a GBV_ILN_4012 | ||
| 912 | |a GBV_ILN_4037 | ||
| 912 | |a GBV_ILN_4112 | ||
| 912 | |a GBV_ILN_4125 | ||
| 912 | |a GBV_ILN_4126 | ||
| 912 | |a GBV_ILN_4249 | ||
| 912 | |a GBV_ILN_4305 | ||
| 912 | |a GBV_ILN_4306 | ||
| 912 | |a GBV_ILN_4307 | ||
| 912 | |a GBV_ILN_4313 | ||
| 912 | |a GBV_ILN_4322 | ||
| 912 | |a GBV_ILN_4323 | ||
| 912 | |a GBV_ILN_4324 | ||
| 912 | |a GBV_ILN_4325 | ||
| 912 | |a GBV_ILN_4335 | ||
| 912 | |a GBV_ILN_4338 | ||
| 912 | |a GBV_ILN_4367 | ||
| 912 | |a GBV_ILN_4700 | ||
| 951 | |a AR | ||
| 952 | |d 2 |j 2023 |e 1 |b 01 |c 02 | ||
| author_variant |
d s ds s k sk h s hs r k rk k k kk h k hk |
|---|---|
| matchkey_str |
article:27314596:2023----::netgtoocreainewetrsadndtmeaueuigrn |
| hierarchy_sort_str |
2023 |
| publishDate |
2023 |
| allfields |
10.1007/s44205-023-00037-y doi (DE-627)SPR049215264 (SPR)s44205-023-00037-y-e DE-627 ger DE-627 rakwb eng Satpathy, Dibyesh verfasserin aut Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2023 Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 Kawabata, Shu aut Sekine, Hokuto aut Kawashima, Rei aut Komurasaki, Kimiya aut Koizumi, Hiroyuki aut Enthalten in Journal of electric propulsion Cham : Springer International Publishing, 2022 2(2023), 1 vom: 01. Feb. (DE-627)1770075232 (DE-600)3092981-7 2731-4596 nnns volume:2 year:2023 number:1 day:01 month:02 https://dx.doi.org/10.1007/s44205-023-00037-y kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2 2023 1 01 02 |
| spelling |
10.1007/s44205-023-00037-y doi (DE-627)SPR049215264 (SPR)s44205-023-00037-y-e DE-627 ger DE-627 rakwb eng Satpathy, Dibyesh verfasserin aut Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2023 Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 Kawabata, Shu aut Sekine, Hokuto aut Kawashima, Rei aut Komurasaki, Kimiya aut Koizumi, Hiroyuki aut Enthalten in Journal of electric propulsion Cham : Springer International Publishing, 2022 2(2023), 1 vom: 01. Feb. (DE-627)1770075232 (DE-600)3092981-7 2731-4596 nnns volume:2 year:2023 number:1 day:01 month:02 https://dx.doi.org/10.1007/s44205-023-00037-y kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2 2023 1 01 02 |
| allfields_unstemmed |
10.1007/s44205-023-00037-y doi (DE-627)SPR049215264 (SPR)s44205-023-00037-y-e DE-627 ger DE-627 rakwb eng Satpathy, Dibyesh verfasserin aut Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2023 Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 Kawabata, Shu aut Sekine, Hokuto aut Kawashima, Rei aut Komurasaki, Kimiya aut Koizumi, Hiroyuki aut Enthalten in Journal of electric propulsion Cham : Springer International Publishing, 2022 2(2023), 1 vom: 01. Feb. (DE-627)1770075232 (DE-600)3092981-7 2731-4596 nnns volume:2 year:2023 number:1 day:01 month:02 https://dx.doi.org/10.1007/s44205-023-00037-y kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2 2023 1 01 02 |
| allfieldsGer |
10.1007/s44205-023-00037-y doi (DE-627)SPR049215264 (SPR)s44205-023-00037-y-e DE-627 ger DE-627 rakwb eng Satpathy, Dibyesh verfasserin aut Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2023 Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 Kawabata, Shu aut Sekine, Hokuto aut Kawashima, Rei aut Komurasaki, Kimiya aut Koizumi, Hiroyuki aut Enthalten in Journal of electric propulsion Cham : Springer International Publishing, 2022 2(2023), 1 vom: 01. Feb. (DE-627)1770075232 (DE-600)3092981-7 2731-4596 nnns volume:2 year:2023 number:1 day:01 month:02 https://dx.doi.org/10.1007/s44205-023-00037-y kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2 2023 1 01 02 |
| allfieldsSound |
10.1007/s44205-023-00037-y doi (DE-627)SPR049215264 (SPR)s44205-023-00037-y-e DE-627 ger DE-627 rakwb eng Satpathy, Dibyesh verfasserin aut Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 2023 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © The Author(s) 2023 Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 Kawabata, Shu aut Sekine, Hokuto aut Kawashima, Rei aut Komurasaki, Kimiya aut Koizumi, Hiroyuki aut Enthalten in Journal of electric propulsion Cham : Springer International Publishing, 2022 2(2023), 1 vom: 01. Feb. (DE-627)1770075232 (DE-600)3092981-7 2731-4596 nnns volume:2 year:2023 number:1 day:01 month:02 https://dx.doi.org/10.1007/s44205-023-00037-y kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 2 2023 1 01 02 |
| language |
English |
| source |
Enthalten in Journal of electric propulsion 2(2023), 1 vom: 01. Feb. volume:2 year:2023 number:1 day:01 month:02 |
| sourceStr |
Enthalten in Journal of electric propulsion 2(2023), 1 vom: 01. Feb. volume:2 year:2023 number:1 day:01 month:02 |
| format_phy_str_mv |
Article |
| institution |
findex.gbv.de |
| topic_facet |
Drift-free-thrust stand Hall thruster Neutral flow Thruster with anode layer |
| isfreeaccess_bool |
true |
| container_title |
Journal of electric propulsion |
| authorswithroles_txt_mv |
Satpathy, Dibyesh @@aut@@ Kawabata, Shu @@aut@@ Sekine, Hokuto @@aut@@ Kawashima, Rei @@aut@@ Komurasaki, Kimiya @@aut@@ Koizumi, Hiroyuki @@aut@@ |
| publishDateDaySort_date |
2023-02-01T00:00:00Z |
| hierarchy_top_id |
1770075232 |
| id |
SPR049215264 |
| language_de |
englisch |
| fullrecord |
<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR049215264</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230510061903.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">230202s2023 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s44205-023-00037-y</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR049215264</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s44205-023-00037-y-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Satpathy, Dibyesh</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2023</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© The Author(s) 2023</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Drift-free-thrust stand</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Hall thruster</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Neutral flow</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Thruster with anode layer</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kawabata, Shu</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Sekine, Hokuto</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kawashima, Rei</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Komurasaki, Kimiya</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Koizumi, Hiroyuki</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of electric propulsion</subfield><subfield code="d">Cham : Springer International Publishing, 2022</subfield><subfield code="g">2(2023), 1 vom: 01. Feb.</subfield><subfield code="w">(DE-627)1770075232</subfield><subfield code="w">(DE-600)3092981-7</subfield><subfield code="x">2731-4596</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:2</subfield><subfield code="g">year:2023</subfield><subfield code="g">number:1</subfield><subfield code="g">day:01</subfield><subfield code="g">month:02</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1007/s44205-023-00037-y</subfield><subfield code="z">kostenfrei</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_11</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_63</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_151</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_170</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_213</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_230</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2014</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4012</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4037</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4112</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4125</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4126</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4249</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4307</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4313</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4322</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4324</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4325</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4335</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4338</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4367</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">2</subfield><subfield code="j">2023</subfield><subfield code="e">1</subfield><subfield code="b">01</subfield><subfield code="c">02</subfield></datafield></record></collection>
|
| author |
Satpathy, Dibyesh |
| spellingShingle |
Satpathy, Dibyesh misc Drift-free-thrust stand misc Hall thruster misc Neutral flow misc Thruster with anode layer Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| authorStr |
Satpathy, Dibyesh |
| ppnlink_with_tag_str_mv |
@@773@@(DE-627)1770075232 |
| format |
electronic Article |
| delete_txt_mv |
keep |
| author_role |
aut aut aut aut aut aut |
| collection |
springer |
| remote_str |
true |
| illustrated |
Not Illustrated |
| issn |
2731-4596 |
| topic_title |
Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 Drift-free-thrust stand (dpeaa)DE-He213 Hall thruster (dpeaa)DE-He213 Neutral flow (dpeaa)DE-He213 Thruster with anode layer (dpeaa)DE-He213 |
| topic |
misc Drift-free-thrust stand misc Hall thruster misc Neutral flow misc Thruster with anode layer |
| topic_unstemmed |
misc Drift-free-thrust stand misc Hall thruster misc Neutral flow misc Thruster with anode layer |
| topic_browse |
misc Drift-free-thrust stand misc Hall thruster misc Neutral flow misc Thruster with anode layer |
| format_facet |
Elektronische Aufsätze Aufsätze Elektronische Ressource |
| format_main_str_mv |
Text Zeitschrift/Artikel |
| carriertype_str_mv |
cr |
| hierarchy_parent_title |
Journal of electric propulsion |
| hierarchy_parent_id |
1770075232 |
| hierarchy_top_title |
Journal of electric propulsion |
| isfreeaccess_txt |
true |
| familylinks_str_mv |
(DE-627)1770075232 (DE-600)3092981-7 |
| title |
Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| ctrlnum |
(DE-627)SPR049215264 (SPR)s44205-023-00037-y-e |
| title_full |
Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| author_sort |
Satpathy, Dibyesh |
| journal |
Journal of electric propulsion |
| journalStr |
Journal of electric propulsion |
| lang_code |
eng |
| isOA_bool |
true |
| recordtype |
marc |
| publishDateSort |
2023 |
| contenttype_str_mv |
txt |
| author_browse |
Satpathy, Dibyesh Kawabata, Shu Sekine, Hokuto Kawashima, Rei Komurasaki, Kimiya Koizumi, Hiroyuki |
| container_volume |
2 |
| format_se |
Elektronische Aufsätze |
| author-letter |
Satpathy, Dibyesh |
| doi_str_mv |
10.1007/s44205-023-00037-y |
| title_sort |
investigation of correlation between thrust and anode temperature during transient operation of raijin-66 |
| title_auth |
Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| abstract |
Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. © The Author(s) 2023 |
| abstractGer |
Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. © The Author(s) 2023 |
| abstract_unstemmed |
Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length. © The Author(s) 2023 |
| collection_details |
GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 |
| container_issue |
1 |
| title_short |
Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66 |
| url |
https://dx.doi.org/10.1007/s44205-023-00037-y |
| remote_bool |
true |
| author2 |
Kawabata, Shu Sekine, Hokuto Kawashima, Rei Komurasaki, Kimiya Koizumi, Hiroyuki |
| author2Str |
Kawabata, Shu Sekine, Hokuto Kawashima, Rei Komurasaki, Kimiya Koizumi, Hiroyuki |
| ppnlink |
1770075232 |
| mediatype_str_mv |
c |
| isOA_txt |
true |
| hochschulschrift_bool |
false |
| doi_str |
10.1007/s44205-023-00037-y |
| up_date |
2024-07-03T23:52:43.069Z |
| _version_ |
1803603948937936896 |
| fullrecord_marcxml |
<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR049215264</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230510061903.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">230202s2023 xx |||||o 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s44205-023-00037-y</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR049215264</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)s44205-023-00037-y-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Satpathy, Dibyesh</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2023</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© The Author(s) 2023</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The thrust performance of RAIJIN-66, a 2 kW-class Thruster with Anode Layer was investigated with respect to anode temperature change at a discharge voltage of 155 V, where propellant was not fully utilized. The upgraded dual pendulum thrust stand used for this study allows for thermal drift free thrust measurement. Correlation between the anode temperature and thrust was measured in real-time before the thruster and stand reached thermal equilibrium. An 8.7% decrease in thrust was reported when the anode temperature increased from 83 ºC to 130 °C. Using an analytical model to elucidate the effect of anode temperature on thruster performance, a good agreement between the predicted and measured thrust values was found for an ionization length of 1.1 mm, but the difference in slope suggests that the thrust performance is more sensitive to the gas temperature than expected. Thrust sensitivity is inferred for conditions in which the ionization mean free path is comparable or greater than the ionization length.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Drift-free-thrust stand</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Hall thruster</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Neutral flow</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Thruster with anode layer</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kawabata, Shu</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Sekine, Hokuto</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Kawashima, Rei</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Komurasaki, Kimiya</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Koizumi, Hiroyuki</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of electric propulsion</subfield><subfield code="d">Cham : Springer International Publishing, 2022</subfield><subfield code="g">2(2023), 1 vom: 01. Feb.</subfield><subfield code="w">(DE-627)1770075232</subfield><subfield code="w">(DE-600)3092981-7</subfield><subfield code="x">2731-4596</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:2</subfield><subfield code="g">year:2023</subfield><subfield code="g">number:1</subfield><subfield code="g">day:01</subfield><subfield code="g">month:02</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1007/s44205-023-00037-y</subfield><subfield code="z">kostenfrei</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_11</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_63</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_151</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_170</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_213</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_230</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2014</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4012</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4037</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4112</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4125</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4126</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4249</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4307</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4313</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4322</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4324</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4325</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4335</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4338</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4367</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">2</subfield><subfield code="j">2023</subfield><subfield code="e">1</subfield><subfield code="b">01</subfield><subfield code="c">02</subfield></datafield></record></collection>
|
| score |
7.397567 |