A passenger compartment, the passenger compartment comprising: a first aircraft seat; a second aircraft seat, the first aircraft seat and the second aircraft seat configured to couple to a floor of an aircraft cabin via a set of seat tracks; a set of floor-mounted components configured to be positioned within the floor separate from the set of seat tracks of the aircraft seat; and a static aircraft seat privacy panel, the static aircraft seat privacy panel comprising: a body; a first surface of the body being shaped to at least partially conform with at least a portion of the first aircraft seat; a second surface of the body being shaped to at least partially conform with at least a portion of the second aircraft seat; a lower edge of the body, the lower edge of the body coupled to the floor via the set of floor-mounted components, the lower edge configured to be positioned proximate to a surface of the floor when the body is coupled to the floor via the set of floor-mounted components; and an upper edge of the body, the upper edge configured to be separated from a surface of one or more overhead structures of the aircraft cabin a selected distance when the body is configured to be coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin, the aircraft seat being compliant with 16G force requirements for aviation transport, the static aircraft seat privacy panel being compliant with 9G force requirements for aviation transport. a first aircraft seat; a second aircraft seat, the first aircraft seat and the second aircraft seat configured to couple to a floor of an aircraft cabin via a set of seat tracks; a set of floor-mounted components configured to be positioned within the floor separate from the set of seat tracks of the aircraft seat; and a static aircraft seat privacy panel, the static aircraft seat privacy panel comprising: a body; a first surface of the body being shaped to at least partially conform with at least a portion of the first aircraft seat; a second surface of the body being shaped to at least partially conform with at least a portion of the second aircraft seat; a lower edge of the body, the lower edge of the body coupled to the floor via the set of floor-mounted components, the lower edge configured to be positioned proximate to a surface of the floor when the body is coupled to the floor via the set of floor-mounted components; and an upper edge of the body, the upper edge configured to be separated from a surface of one or more overhead structures of the aircraft cabin a selected distance when the body is configured to be coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin, a body; a first surface of the body being shaped to at least partially conform with at least a portion of the first aircraft seat; a second surface of the body being shaped to at least partially conform with at least a portion of the second aircraft seat; a lower edge of the body, the lower edge of the body coupled to the floor via the set of floor-mounted components, the lower edge configured to be positioned proximate to a surface of the floor when the body is coupled to the floor via the set of floor-mounted components; and an upper edge of the body, the upper edge configured to be separated from a surface of one or more overhead structures of the aircraft cabin a selected distance when the body is configured to be coupled to one or more structures positioned proximate to a ceiling of the aircraft cabin, the aircraft seat being compliant with 16G force requirements for aviation transport, the static aircraft seat privacy panel being compliant with 9G force requirements for aviation transport.