Test showed that it could carry out the correcting control function according to the trajectory information from the guider head, and the trajectory correction execute mechanism is feasible for infantry rocket grenade.
通过对控制电路的测试,控制电路较好的实现了控制微型脉冲喷气发动机的功能,具有运用在单兵火箭弹道修正的可行性。
参考来源 - 微型脉冲喷气发动机与其控制电路设计及试验·2,447,543篇论文数据,部分数据来源于NoteExpress
应用推荐