Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance
(2018)
Journal Article
Claricoats, J., & Dakka, S. M. (2018). Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance. Aerospace, 5(2), Article 63. https://doi.org/10.3390/aerospace5020063
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 RAVAN (Radiometer Assessment using Vertically Aligned NanoTubes) payloa... Read More about Design of power, propulsion, and thermal sub-systems for a 3U CubeSat measuring Earth’s radiation imbalance.