ROCKET PROPELLANT #2
COMMENTS: This propellant has a burn rate of 0.0385 in/sec at 100 psi and a burn rate of 0.04 in/sec at 300 psi. Burn temperature is approximately 1800K and ISP=180.
PREPARATION (parts by weight):
| CHEMICAL | PERCENT/PARTS | AMOUNT |
| Ammonium nitrate | 0.850 | |
| Elastometric binder (HTPB or other urethane plastic) | 0.150 | |
Total | ||
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