Aerial launch and/or recovery for unmanned aircraft, and associated systems and methods are described. A representative system includes a first, carrier aircraft having an airframe, a propulsion system carried by the airframe and positioned to support the carrier aircraft in hover, and a capture line carried by the carrier aircraft and deployable to hang from the carrier aircraft. The capture line is sized to releasably engage with a capture device of a second, carried aircraft. The system further includes a retrieval device positioned to support the carried aircraft for detachment from the capture line.
AERIAL LAUNCH AND/OR RECOVERY FOR UNMANNED AIRCRAFT, AND ASSOCIATED SYSTEMS AND METHODS
LUFTSTART UND/ODER RÜCKGEWINNUNG VON UNBEMANNTEM LUFTFAHRZEUG UND ZUGEHÖRIGE SYSTEME UND VERFAHREN
LANCEMENT ET/OU RÉCUPÉRATION AÉRIENS POUR AÉRONEF SANS PILOTE, ET SYSTÈMES ET PROCÉDÉS ASSOCIÉS
2023-02-01
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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