The loader is utilized in a guided missile launching system. The rammer forces a missile-booster combination from disengagement with components of a tray of a ready service into engagements with components of a saddle cart and forward and aft floating tracks. The rammer is positioned in one of the trunk sections of a loader, aft of the aft floating track at the loader track level. (Author)
Rammer Mechanism for a Loader
1964
1 pages
Report
No indication
English
NTIS | 1965
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