| Autor: |
Surendran, Sangeetha, Umaiyorupagan, Maheswaran, Renganathan, Thenmozhi, Mathiyalagan, Arun, Singarayan, Rajakumar, Rajarethnam, Subraja |
| Předmět: |
|
| Zdroj: |
AIP Conference Proceedings; 2023, Vol. 2790 Issue 1, p1-4, 4p |
| Abstrakt: |
This research examines current advancements in sophisticated antenna designs for tiny spacecraft (especially CubeSat, etc.). Due to the low-profile requirements, the coupling aperture produces a lot of back radiation. Electromagnetic coupling of radiating element method is used. Cube Satellites, often known as CubeSats, are a type of nano satellite that has recently acquired popularity, particularly among those who see CubeSats as a potential replacement to traditional satellites for space initiatives. This is due to the fact that they are inexpensive and may be constructed using commercial off-the-shelf components [2]. This study examines different antenna designs. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
|
