𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Solid-Fuel Rockets Issue

Book ID
124700451
Publisher
JSTOR
Year
1961
Weight
235 KB
Volume
79
Category
Article
ISSN
0096-4018

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## Abstract The combustion characteristics of variable‐flow ducted rockets were evaluated in order to obtain optimum design parameters of the gas generators. The energetic solid fuels used for the gas generators were glycidyl azide polymer (GAP) with burning rate catalysts. The burning rate of GAP

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