PRESSURIZATION DEVICE FOR ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE AND ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE

PRESSURIZATION DEVICE FOR ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE AND ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE

The present invention relates to the field of liquid rocket technology, and in particular, to a pressurization device for a rocket propelled by liquid oxygen and methane and a rocket propelled by liquid oxygen and methane. The pressurization device for a rocket propelled by liquid oxygen and methane...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: ZHANG, Xi, PENG, Xiaobo, XIONG, Yanbin
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
AVIATION
BLASTING
COMBUSTION ENGINES
COSMONAUTICS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
WEAPONS
Online-Zugang:Volltext bestellen
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
Beschreibung
Zusammenfassung:The present invention relates to the field of liquid rocket technology, and in particular, to a pressurization device for a rocket propelled by liquid oxygen and methane and a rocket propelled by liquid oxygen and methane. The pressurization device for a rocket propelled by liquid oxygen and methane comprises: a liquid oxygen tank provided with a pressurized gas inlet; and a liquid methane tank provided with a pressurized gas cylinder therein, the pressurized gas cylinder being communicated with the pressurized gas inlet through a pipeline. The present invention provides a pressurization device for a rocket propelled by liquid oxygen and methane and a rocket propelled by liquid oxygen and methane with a low cost while ensuring safety.