An improved S-band CubeSat communication subsystem design and implementation
HH Abdullah, A Elboushi, AE Gohar… - IEEE Access, 2021 - ieeexplore.ieee.org
In the past decade, the majority of the launched satellites have a weight exceeds 1 Ton. Its
development takes a long time, high cost, and has a large risk of failure, and does not allow …
development takes a long time, high cost, and has a large risk of failure, and does not allow …
Compact and planar end-fire antenna for PicoSat and CubeSat platforms to support deployable systems
VGG Buendía, SK Podilchak, S Liberto… - IEEE Open Journal …, 2022 - ieeexplore.ieee.org
A miniaturized planar Yagi-Uda antenna for integration with PicoSats or other SmallSat
missions is proposed. Miniaturization techniques, such as meandering and 1-D artificial …
missions is proposed. Miniaturization techniques, such as meandering and 1-D artificial …
Multiband circularly polarised CubeSat antenna operating in S, C, X, Ku, K, and Ka bands
HM Elkady, HH Abdullah… - … Microwaves, Antennas & …, 2024 - Wiley Online Library
A novel design of a high‐frequency multiband with a circular polarisation antenna based on
a four‐patch antenna system consolidated with an Archimedean spiral antenna for CubeSat …
a four‐patch antenna system consolidated with an Archimedean spiral antenna for CubeSat …
[PDF][PDF] Compact and Planar End-fire Antenna for PicoSat and CubeSat Platforms to Support Deployable Systems
TOM WALKINSHAW, C CONSTANTINIDES… - pure.ed.ac.uk
ABSTRACT A miniaturized planar Yagi-Uda antenna for integration with PicoSats or other
SmallSat missions is proposed. Miniaturization techniques, such as meandering and 1-D …
SmallSat missions is proposed. Miniaturization techniques, such as meandering and 1-D …