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 |