Thermal Management System for Spacecraft Thruster

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United States of America Patent

APP PUB NO 20240240622A1
SERIAL NO

18562023

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ATTORNEY / AGENT: (SPONSORED)

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Abstract

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A thermal management system (5) for a magnetoplasmadynamic thruster (10) for a space craft is disclosed. The thermal management system (5) is located between at least one superconducting magnet (120) and a plasma discharge unit (15 and comprises a thermal barrier (40, 60) located adjacent to the plasma discharge unit (15), —a multilayer insulation (70) located between the thermal barrier (40, 60) and the cryostat insulation (80), and a radiation gap (50) located in the thermal barrier (40, 60).

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Patent Owner(s)

Patent OwnerAddress
NEUTRON STAR SYSTEMS DE UGFRANZ-JOSEPH-STR 11 MUNICH 80801

International Classification(s)

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  • 2022 Application Filing Year
  • B64G Class
  • 299 Applications Filed
  • 114 Patents Issued To-Date
  • 38.13 % Issued To-Date
Click to zoom InYear of Issuance% of Matters IssuedCumulative IssuancesYearly Issuances20222023202420250255075100

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Betancourt, Manuel La Rosa Köln, DE 1 0
Chambard, Morgan Köln, DE 1 0
Collier-Wright, Marcus Köln, DE 2 1

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  • B64G Class
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Citation count rangeNumber of patents cited in rangeNumber of patents cited in various citation count ranges144401 - 100102030405060708090100110120130140150160

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