To provide a missile storage system which can stably hold a missile in a vertical direction regardless of the shape and size of the missile.SOLUTION: A storage system 10A of a missile 300 includes: a landing part (a first electrode 67) having a landing surface 45 on which the missile 300 can land; and a storage body 28 for storing the missile 300 landed on the landing surface 45. The storage body 28 has opening/closing parts 42, 44 covering the landing surface 45. The storage system 10A includes holding mechanisms 32, 34 which hold the missile 300 landed on the landing surface 45 in a direction orthogonal to the landing surface 45.SELECTED DRAWING: Figure 1
【課題】飛翔体の形状及びサイズに依らず飛翔体を上下方向に安定して保持することができる飛翔体の格納システムを提供する。【解決手段】飛翔体300の格納システム10Aは、飛翔体300が着地可能な着地面45を有する着地部(第1電極67)と、着地面45に着地した飛翔体300を格納するための格納本体28とを備える。格納本体28は、着地面45を覆う開閉部42、44を有する。格納システム10Aは、着地面45に着地した状態の飛翔体300を着地面45に直交する方向から保持する保持機構32、34を備える。【選択図】図1
MISSILE STORAGE SYSTEM
飛翔体の格納システム
2019-04-25
Patent
Electronic Resource
Japanese
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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