@techreport{oai:jaxa.repo.nii.ac.jp:00047298,
 author = {山田, 健翔 and 内山, 貴啓 and 加藤, 裕之 and 上野, 真 and YAMADA, Kento and UCHIYAMA, Takahiro and KATO, Hiroyuki and UENO, Makoto},
 month = {Jan},
 note = {近年の無人航空機の利用拡大に伴い，将来的に見込まれる無人航空機の性能を明らかにするために，積載量及び航続距離の観点から輸送機械全般のデータをまとめた．結果，積載量1[kg]以上500[kg]以下，航続距離100[km]以上1000[km]以下の範囲に空白領域が確認された．この領域の輸送は無人航空機に適性があり，将来開発される機体の性能要求になると示唆された．また，動力を電動バッテリーとした固定翼機の航続距離を計算し，現状の電動固定翼UAVの空力性能では上記の領域を達成する前に，バッテリーの増量に対して航続距離に限界が出てくることが示唆された．以上から，電動固定翼UAVが将来的に空白領域内の性能を達成するには，電気自動車において内燃機関車に比して空力性能が重要視されているのと同様に，空力性能の研究が重要となるという考察を得た．, With the recent increase in the use of unmanned aerial vehicles (UAVs), data on overall transportation equipment in terms of payload and cruising range were compiled to clarify the performance of unmanned aerial vehicles expected in the future. As a result, a niche was identified for payloads between 1(kg) and 500(kg) and for ranges between 100(km) and 1000(km). It was suggested that this area of transport is suitable for UAVs and will be a performance requirement for future aircraft development. The range of a fixed-wing aircraft powered by an electric battery was calculated, and it was suggested that the current aerodynamic performance of the electric fixed-wing UAVs would be limited by the increase in battery weight before the above range was achieved. These considerations suggest that aerodynamic performance research will be just as important for future electric fixed-wing UAVs to achieve performance within the vacuum region as it is for electric vehicles in comparison to internal combustion engines., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030008000, レポート番号: JAXA-RM-20-003},
 title = {無⼈固定翼機の将来性能に関する潜在ニーズの調査研究},
 year = {2021}
}