Invention Grant
US08350199B2 Apparatus to reduce thrust oscillations in a launch vehicle 有权
用于减少运载火箭中的推力振荡的装置

Apparatus to reduce thrust oscillations in a launch vehicle
Abstract:
A launch vehicle comprising a casing, a solid propellant, a channel, a geometric feature, and a suppression structure. The solid propellant is located within the casing. The channel is through the solid propellant, and the geometric feature is in the channel. The suppression structure is located around a centerline for the channel and located upstream in a flow path from the geometric feature.
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