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.
1. Ratmansky O. I., Krichker I. R. Armature of jet control systems for spacecraft, 136 p. (Mashinostroenie, Moscow, 1980) [in Russian].