Improving the Mechanical Properties of Composite Rocket Propellants
Solid composite rocket propellants usually contain ammoniumperchlorate embedded in an elastic polymer binder. The bindercan be based on a liquid prepolymer such as hydroxyl-terminatedpolybutadiene, HTPB, or poly(3-nitratomethyl-3-methyl oxetane,PolyNIMMO. HTPB is today widely used for this purpose w...
| Main Author: | |
|---|---|
| Format: | Others |
| Language: | English |
| Published: |
KTH, Fiber- och polymerteknologi
2004
|
| Online Access: | http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-1794 http://nbn-resolving.de/urn:isbn:91-7283-742-X |