Transcription of Airframe Structural Materials for Drone Applications
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Airframe Structural Materials for Drone Applications
ARPA ORDER NO.: 189-1. <0. CO. R-581/4-ARPA. July 1971. Airframe Structural Materials for Drone Applications Donald F. Adams D DC. ?MJM. FEB I5 1972. B. A Report prepared for ADVANCED RESEARCH PROJECTS AGENCY. RcprMhicwJ by NATIONAL TECHNICAL. INFORMATION SERVICE. Springflsld, V>. 21151. Rand SANTA MOMCACA. 90406. iN. 51. '. -vll- CONTENTS. i . PREFACE. v SUMMARY. lx TABLES. Section I. INTRODUCTION 1. II. CANDIDATE Materials 3. III. APPLICABILITY TO SPECIFIC MISSIONS 8. IV. TYPICAL Airframe - material COMBINATIONS 15. Aluminum 15. Fiberglass 16. Fiberglass with Paper Honeycomb Core 16. Cast and Molded Plastics 17. Paper and Foam 17. Wood 17. Sall-Wlng Design 18. Graphlte-Fllament/Epoxy Composites 18. Titanium Alloys 18. Other Possibilities 19.
weight of the airframe structure, expressed as a fraction of the gross takeoff weight of the drone vehicle, may be much lower than that for manned aircraft or for highly maneuverable target drones.
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