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ISRO POLYOL - THE VERSATILE BINDER FOR COMPOSITE SOLID PROPELLANTS FOR LAUNCH VEHICLES AND MISSILES.
被引：7
作者：
Krishnamurthy, V.N.
Thomas, Solomon
机构：
关键词：
FLOW OF FLUIDS - Non Newtonian;
D O I：
10.14429/dsj.37.5889
中图分类号：
学科分类号：
摘要：
A family of propellants based on a low cost hydroxy terminated binder has been developed and proved in large size motors. It can meet the requirements of Apogee motors as well as large boosters. The system offers advantages comparable with HTPB propellants in terms of high ballistic performance, stringent mechanical properties, ease and reliability of cure even at ambient conditions and high storage stability. The near-Newtonian flow behavior, simplicity and processing characteristics of this saturated binder propellant are particularly note-worthy.
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页码：29 / 37
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