On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines
|1Shevchenko, SA |
1Yuzhnoye State Design Office, Dnipro, Ukraine
|Kosm. nauka tehnol. 2001, 7 ;(Supplement1):053-057|
|Publication Language: Russian|
An analysis of design peculiarities and utilization of liquid/gas flow control units is presented. The units employ an electromagnet of direct current for a programmed re-tuning instead of an electromechanical actuator. Several schemes and designs of control units of electromagnetic type are considered.
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