Rocket engine cooling and stealth design device

The invention relates to a rocket engine cooling and stealth design device. The rocket engine cooling and stealth design device comprises an engine shell, a combustion chamber, a tail spray pipe, a self-pressurization liquid nitrogen tank, a concentric-square-shaped pipeline and a control component;...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	MAO HONGXIA, WANG ZHENHUA, BAO XINGDONG, XIAO ZHIHE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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