On possibility to use flow control units of electromagnetic type for liquid propellant rocket engines

Heading: 
Space Energy, Power and Propulsion
1Shevchenko, SA
1Yuzhnoye State Design Office, Dnipro, Ukraine
Kosm. nauka tehnol. 2001, 7 ;(Supplement1):053-057
https://doi.org/10.15407/knit2001.01s.053
Publication Language: Russian
Abstract: 
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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References: 
1. Ratmansky O. I., Krichker I. R. Armature of jet control systems for spacecraft, 136 p. (Mashinostroenie, Moscow, 1980) [in Russian].