Comparative study of an additional oxidizer charge effect on selected operational characteristics of a solid-fuel rocket engine

Mariusz Pietraszek,

Tomasz Klemba,

Joanna Lubieniecka,

Jerzy Łukasiewicz,

Jacek Pietraszek

Abstrakt

This paper describes a part of research related to the elimination of adverse phenomenon involving the occurrence of a negative oxygen balance of combustion products of missile engines during their firing from aircrafts. It also presents the results of comparative tests of rocket engines equipped with an additional oxidizer charge.

Słowa kluczowe: oxygen balance, rocket engine, aircraft, oxidizer charge