DocumentCode
1235127
Title
Pathfinder. Developing a solar rechargeable aircraft
Author
Colella, Nicholas J. ; Wenneker, Gordon S.
Author_Institution
Lawrence Livermore Nat. Lab., CA, USA
Volume
15
Issue
1
fYear
1996
Firstpage
18
Lastpage
23
Abstract
Some assignments, both civilian and military, are better performed by unmanned, long-endurance, solar rechargeable aircraft high in the atmosphere than by satellites in low Earth orbits. These aircraft would have more flexible flight paths and would be far less costly than satellites to design, build, and operate. In collaboration with AeroVironment, Inc., the authors developed a lightweight flying wing, called Pathfinder, that uses present-day technologies in photovoltaics, power electronics, aerodynamics, and guidance and control. Because of its light weight, 30 m wingspan, and intended high peak altitude (2025 km), Pathfinder is span loaded; that is, the weight of all components is distributed as evenly as possible across the five modules that make up its wing. Flight tests have proven the soundness of the concepts and components
Keywords
aerospace propulsion; aircraft; aircraft testing; photovoltaic power systems; secondary cells; solar cell arrays; solar cells; 2025 km; 30 m; Pathfinder; aerodynamics; flight control; flight tests; guidance; lightweight flying wing; photovoltaics; power electronics; solar cell modules; solar rechargeable aircraft; Aerodynamics; Aerospace electronics; Aircraft manufacture; Atmosphere; Collaboration; Low earth orbit satellites; Military aircraft; Military satellites; Photovoltaic cells; Power electronics;
fLanguage
English
Journal_Title
Potentials, IEEE
Publisher
ieee
ISSN
0278-6648
Type
jour
DOI
10.1109/45.481371
Filename
481371
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