Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. (Author)
Helicopter External Sling System Basic Vibration Data
1969
11 pages
Report
No indication
English
NTRS | 1980
|Helicopter sling load positioning
Tema Archive | 2009
|Helicopter Sling Load Positioning
British Library Conference Proceedings | 2009
|Helicopter Sling Load Electrical Connector
NTIS | 1970
|