Field Investigation of Gunner Aiming Error as a Function of Launcher Weight
ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL GROUND EQUIPMENT/MATERIALS DIRECTORATE
Pagination or Media Count:
The report presents a field investigation of aiming error as a function of launcher weight and tracking rate for manportable air defense system applications. The effects of launcher weights of 30, 35, 40, 45 and 50 pounds, and tracking rates of below 1, 1 to 4, 4 to 7, and above 7 degreessecond are examined in terms of aiming error at the point of uncage.
- Surface-Launched Guided Missiles
- Human Factors Engineering and Man Machine Systems