CPC B64C 29/0025 (2013.01) [B64C 1/069 (2013.01); B64U 20/40 (2023.01); B64C 2211/00 (2013.01)] | 15 Claims |
1. An aircraft, comprising:
a forward fuselage;
an aft fuselage;
at least one first tube projecting from the forward fuselage and configured to pass through a first channel, wherein the first channel passes through a portion of the aft fuselage;
at least one second tube projecting from the aft fuselage and configured to pass through a second channel, wherein the second channel passes through a portion of the forward fuselage;
a fuel module coupled to fuel a propulsion module of the aircraft, wherein the propulsion module is positioned within a propulsion tail of the aircraft; and
an elevon coupled to the aft fuselage and at least one fourth tube projecting from the elevon and configured to pass through a fourth channel, wherein the fourth channel passes through a second portion of the aft fuselage.
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