Design and fabrication of a 200N thrust rocket motor based on NH4ClO4 + Al + HTPB as solid propellant
The development of rocket motor using potassium nitrate, carbon and sulphur mixture has successfully been developed by researchers and students from UTM and recently a new combination for solid propellant is being created. The new solid propellant will combine a composition of Ammonium perchlorate,...
Saved in:
| Main Authors: | , |
|---|---|
| Format: | Conference or Workshop Item |
| Published: |
2009
|
| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/15034/ https://dx.doi.org/10.1063/1.3464841 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|