AN EXTREMELY SMALL AUTOPHAGE ROCKET FOR ORBITING A PICO SATELLITE

Анотація

A new experiment is the main object of the paper. The experiment continues the series of the tests which are carried-out to clarify the engineering feasibility of an inertial autophage rocket. A distinguish feature of the new test set is a reverse-feed gasification chamber. The successful firing of it is a step towards inertial-pulse engine, the core part of a very small, simple and cheap pocket launch vehicle for pico and femto satellites.