Staged pressurized combustion solid-propellant rocket engine

The invention discloses a staged pressurized combustion solid-propellant rocket engine. The staged pressurized combustion solid-propellant rocket engine comprises a front primary combustion chamber, arear primary combustion chamber, a pressurization chamber and a main combustion chamber which are su...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DONG XINGANG, LI XIAOCONG, LIU PEIJIN, HE GUOQIANG, HE YUANBO, FU BENSHUAI, LIU YANG
Format: Patent
Sprache:chi ; eng
Schlagworte:
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!