Phases I and II of the Integrated Engineering and Service Tests of Prefabricated Aluminum Landing Mats were conducted by the US Army Armor and Engineer Board and US Army General Equipment Test Activity from 15 Aug 66 to 1 Mar 67. Field testing was conducted at Dyess AFB, Texas. The objectives of the test were to determine whether four types of mat, MX19, MX18B, MX18C and AM2 (2-piece, welded), met the requirements of the approved QMR, and their suitability to support AF F-4C, C130, and C-7A aircraft; US Army OV-1 and CH-47 aircraft; and Navy F-4B aircraft.


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    Integrated Engineering and Service Tests of Prefabricated Aluminum Landing Mats

    E. N. Eschbach / J. L. Burchett / R. J. Baeten et al. | NTIS | 1968


    Aluminum scores for landing mats

    Engineering Index Backfile | 1969


    Development of airplane landing mats

    Tolbert, R.L. | Engineering Index Backfile | 1945


    Steel landing mats for airplane runways

    Greulich, G.G. | Engineering Index Backfile | 1943


    Adhoc geo-fiducial mats for landing UAVs

    JOURDAN DAMIEN / SEKINE ANTHONY / VELEZ SCOTT et al. | Europäisches Patentamt | 2023

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