Designing of construction REHF with transversal traction

Аuthors

Knyazev I. A.^1*, Abashev V. M.^2**

1. Machinebuilding Design Bureau”Iskra” named after I.I. Kartukov, 35, Leningradskoe shosse, Moscow, 125284, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: kozlova.iskra@mail.ru
**e-mail: abashevVM@mai.ru

Abstract

Designing engine of hard fuel with transversal vector traction and investigating its intraballistic characteristics.

Keywords:

rocket engine of hard fuel, control system of a traction vector, gas-dynamic calculation, gas stream, area of enhanceable pressure, technological process, boundary and initial conditions.