A review of requirements for gamma radiation detection in space using cubesats

F Arneodo, A Di Giovanni, P Marpu - Applied Sciences, 2021 - mdpi.com
Initially intended as student-led projects at universities and research institutions, the
CubeSats now represent a unique opportunity to access space quickly and in a cost …

Attitude controller design for micro-satellites

MC De Simone, G Ventura, A Lorusso… - International Conference “ …, 2021 - Springer
The increasing interest of private companies in the aerospace sector has produced a growth
of space missions oriented to exploration and colonization. Among the various markets …

Inflatable aerodynamic decelerator for CubeSat reentry and recovery: Altitude effects on the flowfield structure

DR Olave, NC Jara, RC Palharini, RSA Palharini… - Aerospace Science and …, 2023 - Elsevier
In the present investigation, numerical simulations are conducted in order to characterize the
flowfield structure of Inflatable Aerodynamic Decelerators (IAD) for CubeSat reentry and …

[HTML][HTML] Emerging IoT domains, current standings and open research challenges: a review

O Ali, MK Ishak, MKL Bhatti - PeerJ Computer Science, 2021 - peerj.com
Over the last decade, the Internet of Things (IoT) domain has grown dramatically, from ultra-
low-power hardware design to cloud-based solutions, and now, with the rise of 5G …

Inflatable aerodynamic decelerators for CubeSat reentry and recovery: Surface properties

N Caqueo, RC Palharini, RSA Palharini… - Aerospace Science and …, 2024 - Elsevier
Abstract In this investigation, Direct Simulation Monte Carlo Method is used to compute the
surface properties of inflatable aerodynamic decelerators (IAD) applied for the reentry …

Inflatable aerodynamic decelerator for CubeSat reentry and recovery: IAD geometrical effects on the flowfield structure

NC Jara, DR Olave, RC Palharini, E Gaglio… - Aerospace Science and …, 2023 - Elsevier
Abstract In this investigation, Direct Simulation Monte Carlo computations were carried out to
assess the influence of Inflatable Aerodynamic Decelerator (IAD) geometrical configurations …

[HTML][HTML] Decay time estimate for LEO spacecraft

L Niccolai, G Mengali - Acta Astronautica, 2024 - Elsevier
The growing concerns posed by orbital debris represent a serious threat to the future of
space operations in low Earth orbit. With the goal of limiting the formation of new debris …

Dynamically balanced pointing system for CubeSats: study and 3D printing manufacturing

N Sesto Gorella, M Caruso, P Gallina, S Seriani - Robotics, 2021 - mdpi.com
The increasing presence of additive manufacturing (AM) in the space sector prompted us to
investigate the feasibility of a single degree of freedom (DoF) pointing system (PS) made by …

Verification of Space GPS Receiver Navigation Performance Based on Full-Orbit Navigation Solutions of CubeSat

J Park, H Shim, Y Bae, C Kee, S Yu - … Technical Meeting of The Institute of …, 2023 - ion.org
This study verifies navigation performance of in-house developed space GPS receiver using
full-orbit onboard navigation solutions of CubeSat called Seoul National University GNSS …

Progress Towards Controlled Re-entry and Recovery of CubeSats

FW Downey - 2023 - espace.curtin.edu.au
The primary objective of this work was to progress towards performing controlled re-entry
and recovery missions using CubeSats to increase the frequency of Solar System …