Ballistic and mechanical properties of HTPB based composite propellants
β Scribed by M.S. Patil; Haridwar Singh
- Book ID
- 107947079
- Publisher
- Elsevier Science
- Year
- 1988
- Tongue
- English
- Weight
- 563 KB
- Volume
- 19
- Category
- Article
- ISSN
- 0304-3894
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Polyurethanes were synthesized by the reaction of hydroxy-terminated polybutadiene (HTPB) and diisocyanates such as toluene diisocyanate (TDI), diphenylmethane diisocyanate (MDI), hexamethylene diisocyanate (HMDI), and isophorone diisocyanate (IPDI). Carbon black and antimonytrioxide (Sb 2 O 3 ) wer
A polyurethane elastomer having mechanical and adhesive properties suitable for liner applications in solid rocket propellants was developed using HTPB as the prepolymer and IPDI as the curing agent. The effects of the NCO/OH ratio ( R value) and the triol/diol ratio on the mechanical properties of
## Abstract Composite propellants based on hydroxylβterminated polybutadience (HTPB) resin are the most common contemporary solid propellants for launch vehicle and missile applications. A series of HTPB resins, manufactured by freeβradical polymerisation using a peroxide initiator, with varying mo