Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth's radiation imbalance

J Claricoats, SM Dakka - Aerospace, 2018 - mdpi.com
The paper presents the development of the power, propulsion, and thermal systems for a 3U
CubeSat orbiting Earth at a radius of 600 km measuring the radiation imbalance using the …

Static and random vibration analyses of a university CubeSat project

GI Barsoum, HH Ibrahim… - Journal of Physics …, 2019 - iopscience.iop.org
This work presents hands on experience of the configuration process and strength analyses
of a student's CubeSat project at the German University in Cairo. The static and dynamic …

[图书][B] Development and Characterization of the Heated-Anode Cathode Arc Thruster (HA-CAT)

GL Teel - 2014 - search.proquest.com
A modern approach to satellite based experimentation has evolved from large, multi-
instrumented satellites, to cheaper, smaller, almost disposable yet still reliable small …

Investigating Discharge Ignition Fundamentals of Micro-Cathode Arc Thrusters

GL Teel - 2017 - search.proquest.com
This dissertation is a compilation of studies of the volatile process that vacuum arcs undergo,
known as breakdown. Breakdown is a transfer of electrons from one electrode to another …

[PDF][PDF] Access control of NUTS uplink

S Prasai - 2012 - ntnuopen.ntnu.no
Access control of NUTS uplink Page 1 Access control of NUTS uplink Sandesh Prasai Master
of Telematics - Communication Networks and Networked Services (2 Supervisor: Stig Frode …

The Puerto Rico CubeSat project to attract STEM students into the area of aerospace engineering

R Darbali-Zamora, EI Ortiz-Rivera… - 2015 IEEE Frontiers …, 2015 - ieeexplore.ieee.org
The purpose of this paper is to present an interdisciplinary research project in order to attract
engineering students to the area of aerospace systems. The Puerto Rico NASA Space Grant …

I‐2f: Structural Subsystem

KY Şanlıtürk, M Süer, AR Aslan - Nanosatellites: Space and …, 2020 - Wiley Online Library
The structure of a satellite is one of the satellite subsystems, and it is designed to provide a
volume or a 'shelter'where all subsystems are assembled and housed. The primary missions …

[PDF][PDF] Integration of a gps subsystem into the aalto-1 nanosatellite

K Zenger - 2013 - researchgate.net
The thesis begins by introducing the Aalto-1 satellite project, basics of the Global Positioning
System, and satellite tracking with GPS. After this necessary background information, the …

OrbitPlus Open CubeSat Platform Feasibility Study and Preliminary System Design

H Ahmadloo, A Mazinani, S Pourdaraei… - The Proceedings of the …, 2019 - Springer
Following the commercial trend of space sector and taking advantage of smaller satellites to
be launched especially in LEO; OrbitPlus Technology Group began the feasibility study and …

[PDF][PDF] Challenges and Opportunities of Small Satellite Projects as Educational Tools: An Engineering Perspective

M Al-Awani - 2017 - khalifauniversity.elsevierpure.com
Abstract Space exploration through satellite technology has resulted in extensive research
to come up with smaller, lighter and energy efficient satellites. In this regard, CubeSat …