METHOD OF MANUFACTURE OF ROCKET ENGINE SOLID-PROPELLANT CHARGE IGNITER Russian patent published in 2005 - IPC

Abstract RU 2251014 C1

FIELD: rocket engines.

SUBSTANCE: proposed method of manufacture of solid-propellant charge igniter includes vacuum forming of surface of polymeric film case which is carried out directly on seat in rocket engine housing, for instance in engine cover.

EFFECT: improved mass and dimensional characteristics of rocket engine, simplified technology of manufacture.

7 cl, 3 dwg

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RU 2 251 014 C1

Authors

Koz'Jakov A.V.

Molchanov V.F.

Pupin N.A.

Talalaev A.P.

Nikitin V.T.

Mel'Nichenko M.V.

Dates

2005-04-27Published

2003-09-08Filed