FIELD: rocket engine engineering.
SUBSTANCE: charge for solid rocket engine comprises perforated cylindrical grain. The length of some grains is less than that of the charge. The faces of the short grains which face the extensions of the long grains are provided with conical constrictions.
EFFECT: enhanced reliability.
3 cl, 3 dwg
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Authors
Dates
2006-01-20—Published
2004-04-12—Filed