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Structure-property relationship of HTPB-based propellants. II. Formulation tailoring for better mechanical properties

✍ Scribed by R. Manjari; U. I. Somasundaran; V. C. Joseph; T. Sriram

Publisher
John Wiley and Sons
Year
1993
Tongue
English
Weight
531 KB
Volume
48
Category
Article
ISSN
0021-8995

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📜 SIMILAR VOLUMES

Structure-property relationship of HTPB-
Structure-property relationship of HTPB-based propellants. I. Effect of hydroxyl value of HTPB resin
✍ R. Manjari; V. C. Joseph; L. P. Pandureng; T. Sriram 📂 Article 📅 1993 🏛 John Wiley and Sons 🌐 English ⚖ 434 KB 👁 2 views

## Abstract Composite propellants based on hydroxyl‐terminated polybutadience (HTPB) resin are the most common contemporary solid propellants for launch vehicle and missile applications. A series of HTPB resins, manufactured by free‐radical polymerisation using a peroxide initiator, with varying mo

Structure–property relationship of HTPB-
Structure–property relationship of HTPB-based propellants. III. Optimization trials with varying levels of diol–triol contents
✍ R. Manjari; L. P. Pandureng; U. I. Somasundaran; T. Sriram 📂 Article 📅 1994 🏛 John Wiley and Sons 🌐 English ⚖ 401 KB 👁 2 views

A systematic study has been conducted on a composite solid propellant formulation using hydroxyl-terminated polybutadiene ( HTPB ) prepolymer with varying molecular weights and hydroxyl values. Fairly extensive regions of resin parameters have been studied. Contours of important propellant propertie