MOLOT project of hypersonic unmanned launch aircraft with combined shielded turbo-ramjet propulsion system

Аuthors

Makeich G. S.¹, Tukaev M. U.¹, Chibisov Y. N.^2*

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. JSC NPO Molniya,

*e-mail: chibisovyan@bk.ru

Abstract

The research is conducted at the development of a first stage of superlight carry aerospace transportation system - hypersonic unmanned launch aircraft with combined shielded turbo-ramjet propulsion system. Principal research result is a scientific and technical basis of a making possible hypersonic unmanned launch aircraft (March number M = 4.3). This aircraft is a prototype to demonstrate technology of a combined turbo-ramjet propulsion system for a mid carry and heavy carry aerospace transportation system launch aircraft.

Keywords:

hypersonic launch aircraft, combined propulsion system, ramlet, shielded inlet

Download