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.
Integrated Engineering and Service Test of Prefabricated Aluminum Landing Mats
1967
111 pages
Report
Keine Angabe
Englisch
Air Transportation , Landing mats , Acceptability , Performance(Engineering) , Welding , Military requirements , Air force operations , Naval operations , Jet fighters , Transport aircraft , Observation aircraft , Short takeoff aircraft , Helicopters , Drainage , Surface properties , Braking , Life expectancy , Bombing , Landing fields , Aluminum alloys , Skidding , Reflectivity , Light , Dust , Fastenings , Checkout procedures , Am-2 landing mats , C-130 aircraft , C-7 aircraft , F-4 aircraft , H-47 aircraft , Mx-19 landing mats , V-1 aircraft
Aluminum scores for landing mats
Engineering Index Backfile | 1969
Development of airplane landing mats
Engineering Index Backfile | 1945
|Steel landing mats for airplane runways
Engineering Index Backfile | 1943
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