Impact resistant fuselage

An impact resistant fuselage of an aircraft, said fuselage being extended along a central longitudinal direction, wherein transversal sections of the fuselage are comprised in a vertical plane which is perpendicular to the central longitudinal direction, the impact resistant fuselage comprises

• at least one ballistic material membrane extended along the longitudinal direction for absorbing high energy impacts, a transversal section of the ballistic material membrane comprises at least one section between two tensional elements, wherein
• the ballistic material membrane is located inside the fuselage of the aircraft,
• the at least one section of the ballistic material membrane is mechanically linked to the inside of the fuselage by the tensional elements, and
• the two tensional elements stress the ballistic material membrane, and wherein the two tensional elements are end tensional elements which mechanically link the at least one section of the ballistic material membrane to the fuselage at opposite ends of the ballistic material membrane, wherein the ballistic material membrane is connected at the opposite ends to the inside of the fuselage, and
• at least one intermediate tensional element separates a plurality of sections of the ballistic material membrane, and
• said at least one intermediate tensional element is located between a pair of consecutive sections of the ballistic material membrane such that said sections are arranged in a way free to contact each other.