Solid rocket motor propellants with reticulated structures embedded therein to provide variable burn rate characteristics

A solid propellant grain (10) which comprises an homogeneous mass (12) of propellant material including an oxidant. A variable burn rate is provided by embedding a reticulated structure (14) in a portion only of the propellant mass. The reticulated structure may be coated with a high thermal conduct...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SATO, TOMIO, HIGHTOWER, JAMES O. JR
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CHEMISTRY COMBUSTION ENGINES EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MANUFACTURE THEREOF MATCHES MECHANICAL ENGINEERING METALLURGY USE OF SINGLE SUBSTANCES AS EXPLOSIVES WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!