Very-small-satellite design for distributed space missions

170Citations
Citations of this article
140Readers
Mendeley users who have this article in their library.
Get full text

Abstract

A new class of remote sensing and scientific distributed space missions is emerging that requires hundreds to thousands of satellites for simultaneous multipoint sensing. These missions, stymied by the lack of a low-cost massproducible sensor node, can become reality by merging the concepts of distributed satellite systems and terrestrial wireless sensor networks. A novel, subkilogram, very-small-satellite design can potentially enable these missions. Existing technologies are first investigated, such as standardized picosatellites and microengineered aerospace systems. Two new alternatives are then presented that focus on a low-cost approach by leveraging existing commercial mass-production capabilities: a satellite on a chip (SpaceChip) and a satellite on a printed circuit board. Preliminary results indicate that SpaceChip and a satellite on a printed circuit board offer an order of magnitude of cost savings over existing approaches.

Cite

CITATION STYLE

APA

Barnhart, D. J., Vladimirova, T., & Sweeting, M. N. (2007). Very-small-satellite design for distributed space missions. Journal of Spacecraft and Rockets, 44(6), 1294–1306. https://doi.org/10.2514/1.28678

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Save time finding and organizing research with Mendeley

Sign up for free