Pico-Satellite Solar Cell Testbed Qualification Testing

Halpine, John; Liu, S.; Simburger, Edward J.; Yoo, H.; Hinckley, David; Rumsey, Daniel

doi:10.1109/wcpec.2006.279887

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2009

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“…This is due to the physical limitations of the on-board Li-Ion batteries and available area for solar cells [2]. The DC power constraints are critical to CubeSat transceiver design and operation.…”

Section: Figure 1 the Aerocube-2 Cubesatmentioning

confidence: 99%

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CubeSat communications transceiver for increased data throughput

Clark

Chin

Karuza

et al. 2009

2009 IEEE Aerospace Conference

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CubeSat communication links require small size, low power, and low cost transceivers. Link parameters resulting from the satellite's Low Earth Orbit (LEO) can impair transceiver performance, degrading mission data throughput. This paper describes the characteristics and control of a new CubeSat transceiver. The new transceiver provides an estimated 300% increase in data throughput for a typical 45-degree maximum elevation angle LEO pass over the Aerocube-2 transceiver. 12

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Section: Figure 1 the Aerocube-2 Cubesatmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%