Results 1 to 10 of about 30,356 (242)

Optimization of Multi-Mission CubeSat Constellations with a Multi-Objective Genetic Algorithm

open access: yesRemote Sensing, 2023
The increasing demand for low-cost space-borne Earth observation missions has led to small satellite constellation systems development. CubeSat platforms can provide a cost-effective multiple-mission space system using state-of-the-art technology.
Shimeles Demissie Melaku, Hae-Dong Kim
doaj   +2 more sources

Impact observations of asteroid Dimorphos via Light Italian CubeSat for imaging of asteroids (LICIACube). [PDF]

open access: yesNat Commun, 2023
LICIACube as a cubesat for planetary defence LICIACube, constituted by aCubeSatwith dimensions of 10x20x30cm, is the first Italian deep space satellite managed by the Italian Space Agency (ASI).
Dotto E, Zinzi A.
europepmc   +2 more sources

A compact tri-band omnidirectional antenna design for CubeSat applications [PDF]

open access: yesScientific Reports
This paper presents a compact tri-band omnidirectional antenna designed for CubeSat applications, operating at UHF (0.755 GHz), L-band (1.25 GHz), and S-band (2.28–3.74 GHz). The antenna features a defected ground structure (DGS) and metallic vias, which
Rao Shahid Aziz   +2 more
doaj   +2 more sources

Dimensional validation of CubeSat structures using 3D optical scanning technology [PDF]

open access: yesScientific Reports
CubeSat nanosatellites require precise dimensional verification to ensure compatibility with launch systems; however, current validation methods, such as Vernier calipers, are prone to human error and pose risks to satellite systems.
Jhonatan-Fernando Eulopa-Hernandez   +5 more
doaj   +2 more sources

3U CubeSat-Based Hyperspectral Remote Sensing by Offner Imaging Hyperspectrometer with Radially-Fastened Primary Elements. [PDF]

open access: yesSensors (Basel)
This paper presents findings from a spaceborne Earth observation experiment utilizing a novel, ultra-compact hyperspectral imaging camera aboard a 3U CubeSat.
Ivliev N   +11 more
europepmc   +2 more sources

INSPIRE-SAT 7, a Second CubeSat to Measure the Earth’s Energy Budget and to Probe the Ionosphere

open access: yesRemote Sensing, 2022
INSPIRE-SAT 7 is a French 2-Unit CubeSat (11.5 × 11.5 × 22.7 cm) primarily designed for Earth and Sun observation. INSPIRE-SAT 7 is one of the missions of the International Satellite Program in Research and Education (INSPIRE).
Mustapha Meftah   +34 more
doaj   +2 more sources

Use of Solar Panels in the Design of Small CubeSat Spacecraft [PDF]

open access: yesMATEC Web of Conferences, 2021
The article discusses organization of power supply for small spacecraft of CubeSat type. Various methods of power supply of CubeSat onboard equipment are worked out. The use of solar panels (SP) for power supply of CubeSat is proposed.
Selivanov Kirill V.   +2 more
doaj   +1 more source

HYPSO-1 CubeSat: First Images and In-Orbit Characterization

open access: yesRemote Sensing, 2023
The HYPSO-1 satellite, a 6U CubeSat carrying a hyperspectral imager, was launched on 13 January 2022, with the Goal of imaging ocean color in support of marine research. This article describes the development and current status of the mission and payload
Sivert Bakken   +17 more
semanticscholar   +1 more source

CubeSat Communication Subsystems: A Review of On-Board Transceiver Architectures, Protocols, and Performance

open access: yesIEEE Access, 2023
Small satellite communications recently entered a period of massive interest driven by the uprising commercial and civil space applications and motivated by various technological advances.
Amr Zeedan, T. Khattab
semanticscholar   +1 more source

Mission Orbit Design of CubeSat Impactor Measuring Lunar Local [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2017
The current study designs the mission orbit of the lunar CubeSat spacecraft to measure the lunar local magnetic anomaly. To perform this mission, the CubeSat will impact the lunar surface over the Reiner Gamma swirl on the Moon.
Jeong-Ah Lee   +5 more
doaj   +1 more source

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