The power available needs to be balanced with the tasks that need to be completed on the nanocrafts. The radioisotope power sources establish the power budget in the most conservative design. Techniques will be used to switch devices on and off during the mission to optimize the power consumption during various mission stages.
- Barnhart, D. J., Vladimirova, T., and Sweeting, M. N. “Very-small-satellite design for distributed space missions,” Journal of Spacecraft and Rockets, Vol. 44, pp. 1294-1306 (2007)
- Barnhart, D. J., Vladimirova, T., and Sweeting, M. N. “A low-cost femtosatellite to enable distributed space missions,” Acta Astronautica, Vol. 64, pp. 1123-1143 (2009)
- Atchison, J. A. and Peck, M. A. “A passive, sun-pointing, millimeter-scale solar sail,” Acta Astronautica, Vol. 67, pp. 108-121 (2010)
- Manchester, Z. and Peck, M. A. and Filo, A. “KickSat: A Crowd-Funded Mission to Demonstrate the World's Smallest Spacecraft,” Proceedings of the AIAA/USU Conference on Small Satellites (2013)
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