FIELD: armament.
SUBSTANCE: proposed flying vehicle has case with feathering destabilizers provided with counter-weights. Each destabilizer consists of plate changing to attachment unit and feathering limitation unit. Attachment unit is received by hole in nose section of case; its turn is limited within feathering angles x≤40°. Counter-weight is connected with attachment unit.
EFFECT: safe separation from launcher.
20 cl, 10 dwg
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Authors
Dates
2006-11-27—Published
2005-04-22—Filed