Modeling the Dependence of the Specific Impulse on the Temperature of the Heater of an Electrothermal Micro-Motor Based on the Results of Its Tests-Reference-Cited by-同舟云学术

Modeling the Dependence of the Specific Impulse on the Temperature of the Heater of an Electrothermal Micro-Motor Based on the Results of Its Tests

Published:2021-11-01 Issue:1 Volume:2096 Page:012059
ISSN:1742-6588
Container-title:Journal of Physics: Conference Series
language:
Short-container-title:J. Phys.: Conf. Ser.

Author:

Taneeva A S,Lukyanchik V V,Khnyryova E S

Abstract

Abstract The paper investigates the dependence of the specific impulse on the temperature of the heater of an electrothermal micro-motor in order to analyze the possibility of its use as a part of a motion control system for a small technological spacecraft. The possibility of using an electrothermal micro-motor for unloading the angular momentum of flywheel motors is considered.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Link

https://iopscience.iop.org/article/10.1088/1742-6596/2096/1/012059/pdf

Reference19 articles.

1. Alternative solution to increase the duration of microgravity calm period on board the space laboratory;Sedelnikov;Acta Astronautica,2011

2. The usage of fractal quality for microacceleration data recovery and for measuring equipment efficiency check;Sedelnikov;Microgravity Science and Technology,2014

3. Evaluation of calibration accuracy of magnetometer sensors of Aist small spacecraft;Sedelnikov;Journal of Physics: Conference Series,2018

4. «MAKOS-T» A New Spacecraft for Conducting Experiments in Microgravity;Lukiashchenko;Russian Space Bulletin,1996

5. Analysis of the significance of the influence of various components of the disturbance from a temperature shock on the level of microaccelerations in the internal environment of a small spacecraft;Sedelnikov;Microgravity Science and Technology,2021

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