Magnetically-levitated thrust stand for evaluating 6-component thrust vector of 1-N class onboard propulsion devices-Reference-Cited by-同舟云学术

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Magnetically-levitated thrust stand for evaluating 6-component thrust vector of 1-N class onboard propulsion devices

Published:2020-09 Issue: Volume:104 Page:105896
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kakami Akira^ORCID,Hanyu Kosuke,Yano Yasuyuki

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. History of Liquid Propellant Rocket Engines;Sutton,2006

2. Apollo SM-LM RCS engine development program summary report;Hoote,1969

3. Final cassini propulsion system in-flight characterization;Barber,2018

4. Spacecraft Propulsion;Brown,1995

5. The minimum impulse thruster;Parker,2005

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1. Experimental study and performance analysis of a dual-mode space propulsion system pressurized by electric pump;Acta Astronautica;2024-11

2. Performance Validation of the Six-Degree-of-Freedom Thrust Stand Using a Cold Gas Jet Thruster;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2024

3. A combined measurement method of thrust vector and roll torque for low power Hall-effect thrusters;Acta Astronautica;2023-12

4. Absolute displacement measurement using an inertial reference generated by linearised electromagnetic levitation;Mechanical Systems and Signal Processing;2023-04

5. A three-dimensional numerical study on the effect of geometric asymmetry on arcjet thruster performance;Plasma Science and Technology;2023-02-22

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