Wireless Power Transfer to Sitallite Stratospheric Platform

Stratospheric superpressure balloons are a class of high-altitude pseudo-satellite (HAPS) with excellent observational and communications capabilities. The challenge to long-duration operation is station keeping against the thin but fast zephyrs at altitudes around 25 km. One solution is captured in...

Full description

Saved in:
Bibliographic Details
Published inIEEE International Conference on Wireless for Space and Extreme Environments conference digest (Online) pp. 130 - 134
Main Authors Schubert, Peter J., van Wynsberghe, Erinn, Kragt Finnell, Abigail J., Salgueiro, Cristian, Suri, Ramaa Saket
Format Conference Proceeding
LanguageEnglish
Published IEEE 12.10.2020
Subjects
Online AccessGet full text

Cover

Loading…
More Information
Summary:Stratospheric superpressure balloons are a class of high-altitude pseudo-satellite (HAPS) with excellent observational and communications capabilities. The challenge to long-duration operation is station keeping against the thin but fast zephyrs at altitudes around 25 km. One solution is captured in the US patent 10,404,353, which describes a "Sitallite" HAPS having plasma air thrusters to maneuver against the wind. To hold station for months at a time requires a steady delivery of power, such as a microwave beam transmitted from a terrestrial phased array antenna (PAA) to a rectifying receiving antenna (rectenna) mounted on the underside of the superpressure balloon. This work explores the design and safety considerations for the wireless power transfer (WPT) aspects of such a Sitallite and the tradeoffs between array sizes and power requirements. Presented here are studies of the directivity of the PAA as a function of the number and spacing of antenna elements, and the expected impact on ground personnel, insects, birds, and overflying aircraft. The support and suspension structure of the high-altitude rectenna are developed, along with a comparison of various commercial Schottky diodes for this application. Finally, system studies are presented to illustrate the cost drivers and size optimization. Such a Sitallite can provide line-of-sight visibility for a 1,100 km radius, remain aloft for many months, and provide services normally expected from an orbiting satellite at a fraction of the cost.
ISSN:2380-7636
DOI:10.1109/WiSEE44079.2020.9262657