A fairing assembly (114A) for an aerial vehicle (100) having a tank (202) that forms a body (110) of the vehicle and a wing (112) coupled to the tank is provided. The fairing assembly includes a substructure (164) configured to couple with a tank skin (378) of the tank, a thermal protection system (190) coupled to the substructure, and a seal assembly (192) coupled to the substructure, the seal assembly being configured to overlap at least a portion of an edge (118) of the wing.
FAIRING ASSEMBLY AND METHOD THEREFOR
VERKLEIDUNGSANORDNUNG UND VERFAHREN DAFÜR
ASSEMBLAGE DE CARÉNAGE ET SON PROCÉDÉ
2021-05-12
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |