Abstract Small satellites, weighting between 100 and 200kg, have witnessed increasing use for a variety of space applications including remote sensing constellations and technology demonstrations. The energy storage/stored power demands of most spacecraft, including small satellites, are currently accommodated by rechargeable batteries—typically nickel–cadmium cells (specific energy of 50Whkg⁻¹), or more recently lithium-ion cells (150Whkg⁻¹). High energy density is a primary concern for spacecraft energy storage design, and these batteries have been sufficient for most applications. However, constraints on the allowable on-board battery size have limited peak power performance such that the maximum power supply capability of small satellites currently ranges between only 70 and 200W. This relatively low maximum power limits the capabilities of small satellites in terms of payload design and selection. In order to enhance these satellites' power performance, the research reported in this paper focused on the implementation of super-capacitors as practical rechargeable energy storage medium, and as an alternative to chemical batteries. Compared to batteries, some super-capacitors are able to supply high power at high energy-efficiency, but unfortunately they still have a very low energy density (5–30Whkg⁻¹). However, the provision of this high power capability would considerably widen the range of small satellite applications.

Highlights ► Highlighted major issues need to be tackled. ► Presented survey of conventional platforms and determined requirements. ► Determined feasibility and effectiveness of using super-capacitor on small-satellites. ► Derived a formula for estimating discharging efficiency. ► The super-capacitor can replace an on-board battery and provide high power capability.