COOLING SYSTEM FOR ROCKET MOTOR

PURPOSE:To obtain big cooling effect by substituting ablative shielding material for one part or total of conventional fibrous insulator, and utilizing the heat insulating surface for a heat radiating surface after combustion. CONSTITUTION:In the case of heat radiation of a rocket motor 4, 5 of whic...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	SHINOZAKI TAKAO
Format:	Patent
Sprache:	eng
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
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