Proceedings of the 2nd International Conference on Aviation Industry, Education, and Regulation, AVINER 2023, 8-9 November 2023, Jakarta, Indonesia

Research Article

Anti-Ship Missiles Carrier Wing In Ground (WIG) Aircraft

Download32 downloads
  • @INPROCEEDINGS{10.4108/eai.8-11-2023.2345856,
        author={EK  Alimin and CA  Listia},
        title={Anti-Ship Missiles Carrier Wing In Ground (WIG) Aircraft},
        proceedings={Proceedings of the 2nd International Conference on Aviation Industry, Education, and Regulation, AVINER 2023, 8-9 November 2023, Jakarta, Indonesia},
        publisher={EAI},
        proceedings_a={AVINER},
        year={2024},
        month={5},
        keywords={missile carrier aircraft stealth wing in ground effect},
        doi={10.4108/eai.8-11-2023.2345856}
    }
    
  • EK Alimin
    CA Listia
    Year: 2024
    Anti-Ship Missiles Carrier Wing In Ground (WIG) Aircraft
    AVINER
    EAI
    DOI: 10.4108/eai.8-11-2023.2345856
EK Alimin1,*, CA Listia1
  • 1: Aerospace University of Air Marshal Suryadarma
*Contact email: ealimin@yahoo.com

Abstract

A small stealth Wing-In Ground (WIG) aircraft with one crewman carries two anti ship missiles that is designed to fulfil a role of the anti-ship defense system. Because ship defence is based on radar and infrared sensor, it must be capable to avoid both detections. The aircraft has range of 500 km with maximum take-off weight 4500 kg, cruise speed 160 km/hour and payload 750 kg. Its conceptual design follows a procedure from existing design method. It covers wing geometry, power loading, wing loading, sizing, layout, aerodynamic, propulsion, weight, pitching stability, trimmed analysis, and aerodynamic simulation. Besides, by flying low, detection distance between aircraft and ship radars can be reduced. In order to increase anti- ship capability, stealth capability is added and is fulfilled by anti-radar and reduction infared detection. Anti-radar capability is fulfilled by the aircraft configuration designed based on wing-fuselage blended, placement engines and missiles inside the fuselage, and the V-tail. This typical configuration can avoid reflection from radar beam. Capability to reduce infrared detection is fulfilled by concealing the exhaust. Three-dimensional digital based aircraft configuration that is designed by using CAD software is already completed.