382062

Optimal thermal design parameters of educational remote sensing satellite.

Article

Last updated: 04 Jan 2025

Subjects

-

Tags

Environmental Engineering

Abstract

Abstract
Remote sensing satellites are like space mirrors that help map land use, monitor disasters, and track environmental changes. They provide valuable data for various applications, from urban planning to climate research. The problem is that space temperatures vary drastically, ranging from 120°C in direct sunlight due to the Sun's intense radiation. This condition is called worst-case hot temperature —since there is no atmosphere to block or moderate it—to as low as -180°C when in Earth's shadow, and this is called worst-case cold temperature. Satellites are equipped with electronic systems that must function within specified temperature limits (from -10°C to 50°C) over their operational lifespans, making it essential to manage thermal conditions to maintain these limits. To address this issue, we used a thermal control system (both passive and active), which will be discussed further in this paper. However, there is a research and knowledge gap in the literature addressing the design and control of remote-sensing satellites in low Earth orbit. This investigation aims to fill this knowledge gap by developing a comprehensive thermal analysis and thermal control model for the "Space Sight MED 2025" remote sensing satellite in low Earth orbit. The developed computational thermal analysis clearly defines the satellite subsystems' worst-case hot and cold temperatures. Two extreme scenarios of extreme hot and extreme cold sun fluxes were considered in a passive system mode. The radiators' areas, temperatures, and locations on the satellite panels were analyzed under the hot scenario. At the same time, the power and operating conditions of the heaters were evaluated based on the cold scenario. Five heaters, each with an 8-watt power rating of 40 watts. Results showed that the 0.5871m² of radiator area is required. The temperatures of the electronic and electrical equipment should range from −7°C to+40°C. However, due to its high sensitivity to temperature changes, the battery should be kept in lower temperatures from 2°C to +28°C.

DOI

10.21608/auber.2024.319251.1090

Keywords

THERMAL, remote, design, coating

Authors

First Name

Ahmed

Last Name

Abdelbary

MiddleName

Farag

Affiliation

كلية الهندسة جامعة السويس قسم الهندسة الميكانيكية

Email

ahmed-abdelbary@eng.suezuni.edu.eg

City

السويس

Orcid

-

Volume

27

Article Issue

2

Related Issue

47994

Issue Date

2024-10-01

Receive Date

2024-09-09

Publish Date

2024-10-01

Page Start

41

Page End

59

Print ISSN

1110-6107

Online ISSN

2735-3559

Link

https://auber.journals.ekb.eg/article_382062.html

Detail API

https://auber.journals.ekb.eg/service?article_code=382062

Order

382,062

Type

Original Article

Type Code

1,354

Publication Type

Journal

Publication Title

Assiut University Bulletin for Environmental Researches

Publication Link

https://auber.journals.ekb.eg/

MainTitle

Optimal thermal design parameters of educational remote sensing satellite.

Details

Type

Article

Created At

26 Dec 2024