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Development of a Cold Gas Propulsion System for a 1u Cube Satellite.

紀錄類型:	書目-語言資料,手稿 : Monograph/item
正題名/作者:	Development of a Cold Gas Propulsion System for a 1u Cube Satellite./
作者:	Perea, Norma Alicia.
面頁冊數:	1 online resource (53 pages)
附註:	Source: Masters Abstracts International, Volume: 82-04.
Contained By:	Masters Abstracts International82-04.
標題:	Aerospace engineering. -
電子資源:	click for full text (PQDT)
ISBN:	9798672169064

Development of a Cold Gas Propulsion System for a 1u Cube Satellite.
Perea, Norma Alicia.

Development of a Cold Gas Propulsion System for a 1u Cube Satellite. - 1 online resource (53 pages)

Source: Masters Abstracts International, Volume: 82-04.

Thesis (M.S.)--The University of Texas at El Paso, 2020.

Includes bibliographical references

In efforts to further the development test capabilities of nanosatellites on earth, NASA White Sands Test Facility (WSTF) is developing a Magnetic Levitation Table (MLT) for ground testing of nanosatellites. Testing of the table requires dedicated test articles that employ space-like systems, but those that can be used in the confines of a small lab testing area. In collaboration with WSTF, the University of Texas at El Paso (UTEP) Center for Aerospace Exploration Technology Research (cSETR) is developing an 1U cold gas propulsion cube-satellite demonstrator (CGD) to test capabilities of the levitation table. A 1U cube satellite was designed with a cold gas propulsion system. The cold gas demonstrator, weighing 1.5kg, uses cold gas thruster configuration. The CGD uses refrigerant R-134a as the propellant as it is stored in liquid state requiring a lower fill pressure and maximizes the propellant quantity. Four thrusters are placed to provide uniaxial translation around the x-axis and rotation about the y-axis. Movement of the CGD is controlled by throttling miniature solenoid valves that feed directly to the thrusters. This work outlines the development of an integrated, self-contained propulsion unit dedicated for use as a ground-based attitude control test bed demonstrator.

Electronic reproduction.
Ann Arbor, Mich. :
ProQuest,
2024

Mode of access: World Wide Web

ISBN: 9798672169064Subjects--Topical Terms:

686400
Aerospace engineering.
Subjects--Index Terms:

Cold GasIndex Terms--Genre/Form:

554714
Electronic books.

Development of a Cold Gas Propulsion System for a 1u Cube Satellite.
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504 $a Includes bibliographical references
520 $a In efforts to further the development test capabilities of nanosatellites on earth, NASA White Sands Test Facility (WSTF) is developing a Magnetic Levitation Table (MLT) for ground testing of nanosatellites. Testing of the table requires dedicated test articles that employ space-like systems, but those that can be used in the confines of a small lab testing area. In collaboration with WSTF, the University of Texas at El Paso (UTEP) Center for Aerospace Exploration Technology Research (cSETR) is developing an 1U cold gas propulsion cube-satellite demonstrator (CGD) to test capabilities of the levitation table. A 1U cube satellite was designed with a cold gas propulsion system. The cold gas demonstrator, weighing 1.5kg, uses cold gas thruster configuration. The CGD uses refrigerant R-134a as the propellant as it is stored in liquid state requiring a lower fill pressure and maximizes the propellant quantity. Four thrusters are placed to provide uniaxial translation around the x-axis and rotation about the y-axis. Movement of the CGD is controlled by throttling miniature solenoid valves that feed directly to the thrusters. This work outlines the development of an integrated, self-contained propulsion unit dedicated for use as a ground-based attitude control test bed demonstrator.
533 $a Electronic reproduction. $b Ann Arbor, Mich. : $c ProQuest, $d 2024
538 $a Mode of access: World Wide Web
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653 $a Refrigerant
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