Results 1 to 10 of about 19,619 (213)
CubeSat Mission: From Design to Operation
The current success rate of CubeSat missions, particularly for first-time developers, may discourage non-profit organizations to start new projects.
Cristóbal Nieto-Peroy, M Reza Emami
exaly +3 more sources
A compact tri-band omnidirectional antenna design for CubeSat applications. [PDF]
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
Aziz RS +2 more
europepmc +2 more sources
Daily Retrieval of NDVI and LAI at 3 m Resolution via the Fusion of CubeSat, Landsat, and MODIS Data
Constellations of CubeSats are emerging as a novel observational resource with the potential to overcome the spatiotemporal constraints of conventional single-sensor satellite missions.
Rasmus Houborg, Matthew F. McCabe
exaly +3 more sources
Dimensional validation of CubeSat structures using 3D optical scanning technology. [PDF]
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.
Eulopa-Hernandez JF +5 more
europepmc +2 more sources
Use of Solar Panels in the Design of Small CubeSat Spacecraft [PDF]
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
Mission Orbit Design of CubeSat Impactor Measuring Lunar Local [PDF]
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
INSPIRE-SAT 7, a Second CubeSat to Measure the Earth’s Energy Budget and to Probe the Ionosphere
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 +1 more source
Optimization of Multi-Mission CubeSat Constellations with a Multi-Objective Genetic Algorithm
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 +1 more source
Naphthalene as a Cubesat Cold Gas Thruster Propellant
The “cubesat” form factor (multiples of 10 × 10 × 10 cm3 volume and 1.33 kg mass) has been adopted as the defacto standard for a cost effective and modular, nano-satellite platform.
Dimitrios Tsifakis +2 more
doaj +1 more source
In this study, a new spiral dual-band antenna integrated with an optical system for a small CubeSat spacecraft was proposed. It is challenging to design an antenna with a limited space on a CubeSat platform.
Nursultan Meirambekuly +6 more
doaj +1 more source

