Essays about: "cubesat structure"

Showing result 1 - 5 of 14 essays containing the words cubesat structure.

  1. 1. Vibration analysis and testing of a 6U cubesat propulsion system

    University essay from KTH/Lättkonstruktioner, marina system, flyg- och rymdteknik, rörelsemekanik

    Author : Likitha Thimmaraju Girijadevi; [2023]
    Keywords : 6U CubeSat; Propulsion system; Vibration testing; COMSOL; Structures; ECSS; Stress; Resonance; Frequency; Load; Simulation.; 6U CubeSat; Framdrivningssystem; Vibrationstestning; COMSOL; Strukturer; ECSS; Stress; Resonans; Frekvens; Belastning; Simulering.;

    Abstract : Space industry has been booming in the recent times, investments have not justbeen made on satellites and launch vehicles but also on space sustainability. Spaceindustry has its users in national agencies, private commercial agencies, academia andexperimental organisations. READ MORE

  3. 2. Thermal environment and design considerations of the Foresail-2 satellite mission

    University essay from Luleå tekniska universitet/Rymdteknik

    Author : Deepa Anantha Raman; [2023]
    Keywords : satellite; thermal control; radiation; heat transfer; boom;

    Abstract : The thermal design of small satellite missions is critical for ensuring the performance and longevity of onboard instruments. This thesis focuses on the thermal design of Foresail-2, a 6U CubeSat mission to Geostationary Transfer Orbit (GTO), specifically addressing the thermal challenges associated with the magnetometer located at the end of a long boom featured on the satellite. READ MORE

  4. 3. Development of the UnoSat Platform for stratospheric balloon payloads

    University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknik

    Author : Sebastian Scholz; [2023]
    Keywords : Arduino; Stratospheric balloon;

    Abstract : The UnoSat Platform is a software and 3D structure platform built with Arduino Uno boardsthat allows easier implementation of a satellite project in a 1-n unit CubeSat format. It isdesigned to improve and speed up development of balloon - nanosat projects of the M2 TSImaster. READ MORE

  5. 4. Radiation Shielding Simulations for Small Satellites on Geostationary Transfer Orbit

    University essay from Luleå tekniska universitet/Institutionen för system- och rymdteknik

    Author : Anton Fetzer; [2022]
    Keywords : GTO; Foresail-2; CubeSat; Radiation Shielding; Geant4; Radiation Belts; GTO; Foresail-2; CubeSat; säteilysuojaus; Geant4; säteilyvyöhyke;

    Abstract : The emergence of small and affordable satellites has led to rapid growth in the number of launched satellites over the past two decades. To save costs, small satellites often use mass-produced electronic components not explicitly designed for the radiation environment of space, which reduces reliability and makes them unsuitable for higher orbits. READ MORE

  6. 5. Design of a variable focal length optics for a SWIR Earth observation camera

    University essay from Luleå tekniska universitet/Rymdteknik

    Author : Sergio David Díaz Martínez; [2021]
    Keywords : ;

    Abstract : This thesis consists of a preliminary design study of a variable focal length optics for a SWIREarth observation camera which is planned to be placed inside a 6U Cubesat. After thesuccess of DRAGO instrument consisting on a SWIR camera onboard a Cubesat, which hasbeen recently launched (January 2021), the Institute of Astrophysics of the Canary Islands(IAC) began this project with the intention of adding zoom optics to SWIR space imagingsystems. READ MORE