Thrust stand based on a single point load cell for impulse measurements from plasma thrusters-Reference-Cited by-同舟云学术

Thrust stand based on a single point load cell for impulse measurements from plasma thrusters

Published:2020-02-01 Issue:2 Volume:91 Page:023308
ISSN:0034-6748
Container-title:Review of Scientific Instruments
language:en
Short-container-title:Review of Scientific Instruments

Author:

Conde L.¹^ORCID,Lahoz M. D.¹,Grabulosa J.¹,Hernández R.¹,González J.¹^ORCID,Delgado M.¹,Damba J.¹^ORCID

Affiliation:

1. Department of Applied Physics, Escuela Técnica Superior de Ingeniería Aeronáutica y del Espacio, Universidad Politécnica de Madrid, 28040 Madrid, Spain

Funder

Aernnova Aerospace S.A.

Ministerio de Ciencia, Innovación y Universidades

Publisher

AIP Publishing

Subject

Instrumentation

Link

http://aip.scitation.org/doi/pdf/10.1063/1.5127189

Reference13 articles.

1. Electric propulsion for satellites and spacecraft: established technologies and novel approaches

2. Plasmas for space propulsion

3. Plasmas for spacecraft propulsion

4. Fundamentals of Electric Propulasion

5. Electric propulsion for small satellites

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1. Impulse Measurement Methods for Space Micro-Propulsion Systems;Propulsion Systems - Recent Advances, New Perspectives and Applications;2023-10-11

2. Thrust measurements and mesothermal plasma plume of the Alternative Low Power Hybrid Ion Engine (alphie);Journal of Electric Propulsion;2022-11-14

3. Physics of the high specific impulse alternative low power hybrid ion engine (alphie): Direct thrust measurements and plasma plume kinetics;Journal of Applied Physics;2022-01-14

4. Comparison of Submillinewton Thrust Measurements Between a Laser Interferometer and a Load Cell on a Pendulum Balance;Frontiers in Space Technologies;2021-04-27