SOLID-PROPELLANT CHARGE Russian patent published in 2000 - IPC

Abstract RU 2150599 C1

FIELD: space engineering. SUBSTANCE: solid-propellant charge has body, protective securing layer, star-shaped passage in bottom section of charge, adapter and cylindrical sections. Cylindrical section of passage has diameter equal to outer diameter of beams of star-shaped passage at end of transient section. Minimum area of flow section of star-shaped passage range from 0.004 to 0.005 of area of burning section of star-shaped passage as far as indicated section. Initial thickness of burning dome of charge in area of star-shaped passage at bottom end face ranges from 0.85 to 0,95e2, where e2 - is initial thickness of burning dome of charge in area of star-shaped passage at the beginning of transient section. EFFECT: increased coefficient of volumetric load at reduced spread in power characteristics. 2 dwg

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Authors

Makarovets N.A.

Denezhkin G.A.

Semilet V.V.

Podchufarov V.I.

Obozov L.I.

Kashirkin A.A.

Peturkin D.M.

Filatov V.G.

Kuksenko A.F.

Kuz'Mitskij G.Eh.

Fedchenko N.N.

Vronskij N.M.

Makarov L.B.

Grinberg S.I.

Talalaev A.P.

Kolesnikov V.I.

Amarantov G.N.

Kolach P.K.

Nekrasov V.I.

Dates

2000-06-10Published

1999-10-14Filed