Abstract
While there are many different challenges in the development of micro aerial vehicles (MAV), one of the severe limiting factors in terms of weight is the energy storage/power system. Most of the MAVs developed to date are based on electrochemical batteries coupled with an electric motor. In a previous study, several potential alternative energy storage/power systems were examined, evaluated for their specific energy and specific power, and compared to electrical batteries and hydrocarbon fuel storage. Additionally, the power and energy requirements of fixed wing MAV and rotary wing MAV were calculated, for comparison with the different alternatives. In the present study a novel PCM open cycle storage/power system for MAV applications is proposed, based on those requirements. It is an open cycle that uses the ambient temperature as its hot reservoir. Promising initial results, in terms of specific power (45-70W/kg), specific energy (24-45W-hr/kg) and open-cycle thermodynamic efficiency (22-54%), are presented.
| Original language | English |
|---|---|
| Title of host publication | 54th Israel Annual Conference on Aerospace Sciences 2014 |
| Publisher | Technion – Israel Institute of Technology |
| Pages | 928-943 |
| Number of pages | 16 |
| ISBN (Print) | 9781632662651 |
| State | Published - 1 Jan 2014 |
| Externally published | Yes |
| Event | 54th Israel Annual Conference on Aerospace Sciences, IACAS 2014 - Tel-Aviv and Haifa, Israel Duration: 19 Feb 2014 → 20 Feb 2014 |
Publication series
| Name | 54th Israel Annual Conference on Aerospace Sciences 2014 |
|---|---|
| Volume | 2 |
Conference
| Conference | 54th Israel Annual Conference on Aerospace Sciences, IACAS 2014 |
|---|---|
| Country/Territory | Israel |
| City | Tel-Aviv and Haifa |
| Period | 19/02/14 → 20/02/14 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
ASJC Scopus subject areas
- Aerospace Engineering
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