SOME PRINCIPLES DESIGN WORK FOR BIPROPELLANT LIQUID ROCKET ENGINE OF THE SMALL THRUST.

摘要

Two principles -"Quality of design" and "Controlability of the working process" are proposed for design work. As example design work of bipropellant Liquid Rocket Engines of the Small Thrust (LREST) with use of this principles is demonstrated. Two design of mixing head for LREST -"circular wedge" and "lamellar head" - are analyzed. The used diapasons of this design are recommended.