Static testing was performed on an H-777 container to determine its acceptability for carrying the SRAM payload in cargo aircraft. Several suitable tiedown configurations were devised and successfully tested. The base and side of the container suffered some permanent deformation at 6.72 g laterally. Yielding of the simulated internal suspension system occurred at 6.88 g longitudinally. (Author)
Tiedown Tests of The Modified H-777 as a SRAM Payload Section Container
1973
44 pages
Report
Keine Angabe
Englisch
Manufacturing Processes & Materials Handling , Missile Technology , Logistics Military Facilities & Supplies , Containers , Air transportation , Air to surface missiles , Payload , Transport aircraft , Chains , Attachment , Assembly , Steel , Aluminum , Load distribution , Friction , Acceleration , Deformation , Deceleration , Buckling , C-130 aircraft , C-141 aircraft , H-777 containers , Short range air missiles , Sram(Short range air missiles) , Tiedowns
NTRS | 1982
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