Space thermo acoustic radio-isotopic power system: Space trips

A. Breķis; J. E. Freibergs; A. Alemany

doi:10.22364/mhd.55.1-2.1

Space thermo acoustic radio-isotopic power system: Space trips

A. Breķis
, J. E. Freibergs
, A. Alemany^*

^*Šī darba korespondējošais autors

Fizikas institūts

Riga Technical University
University of Latvia
ENSHMG

Zinātniskās darbības rezultāts: Devums žurnālam › Zinātniskais raksts (žurnālā) › koleģiāli recenzēts

9 Atsauces (Scopus)

Kopsavilkums

The paper presents experimental results on testing a travelling wave thermoacoustic (TAc) engine using argon gas coupled with a 200W, low-power, magnetohydrodynamic (MHD) gene- rator using liquid sodium. The project is a terrestrial test and simulation of a radio isotopic- fed electrical power supply system for deep space applications. A large range of parameters were analyzed, such as TAc generated pressure oscillation amplitude as a function of the mean pressure and temperature of the heater.

Oriģinālvaloda	Angļu
Lapas (no-līdz)	5-14
Lapu skaits	10
Žurnāls	Magnetohydrodynamics
Sējums	55
Izdevuma numurs	1-2
DOIs	https://doi.org/10.22364/mhd.55.1-2.1
Publikācijas statuss	Publicēts - 2019

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title = "Space thermo acoustic radio-isotopic power system: Space trips",

abstract = "The paper presents experimental results on testing a travelling wave thermoacoustic (TAc) engine using argon gas coupled with a 200W, low-power, magnetohydrodynamic (MHD) gene- rator using liquid sodium. The project is a terrestrial test and simulation of a radio isotopic- fed electrical power supply system for deep space applications. A large range of parameters were analyzed, such as TAc generated pressure oscillation amplitude as a function of the mean pressure and temperature of the heater.",

author = "A. Breķis and Freibergs, \{J. E.\} and A. Alemany",

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doi = "10.22364/mhd.55.1-2.1",

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T2 - Space trips

AU - Breķis, A.

AU - Freibergs, J. E.

AU - Alemany, A.

PY - 2019

Y1 - 2019

N2 - The paper presents experimental results on testing a travelling wave thermoacoustic (TAc) engine using argon gas coupled with a 200W, low-power, magnetohydrodynamic (MHD) gene- rator using liquid sodium. The project is a terrestrial test and simulation of a radio isotopic- fed electrical power supply system for deep space applications. A large range of parameters were analyzed, such as TAc generated pressure oscillation amplitude as a function of the mean pressure and temperature of the heater.

AB - The paper presents experimental results on testing a travelling wave thermoacoustic (TAc) engine using argon gas coupled with a 200W, low-power, magnetohydrodynamic (MHD) gene- rator using liquid sodium. The project is a terrestrial test and simulation of a radio isotopic- fed electrical power supply system for deep space applications. A large range of parameters were analyzed, such as TAc generated pressure oscillation amplitude as a function of the mean pressure and temperature of the heater.

UR - https://www.scopus.com/pages/publications/85067309801

U2 - 10.22364/mhd.55.1-2.1

DO - 10.22364/mhd.55.1-2.1

M3 - Article

AN - SCOPUS:85067309801

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IS - 1-2

ER -

Space thermo acoustic radio-isotopic power system: Space trips

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