FIELD: rocket fuels.
SUBSTANCE: invention relates to inserted charges of solid rocket fuels largely used in various-destination rocket systems. Method comprises pouring armoring composition into gap between charge to be armored and cartridge under the action of centrifugal force directed along annular gap and creating overload at the inlet of gap at last 60 g. Armoring composition constituents are continuously measured out, mixed, and conveyed to mold rotating together with disk, to which several such molds are peripherally attached. To facilitate armoring composition flow into the gap and to degas composition, mold is given vacillating motion with predetermined amplitude and frequency.
EFFECT: improved quality of charge coating.
3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
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