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Rocket Propellant Properties: solid db ap hmx al
Rocket propellant performance data — specific impulse, characteristic velocity, chamber conditions for bipropellant, solid, and monopropellant combinations
| propellant id | density g cm3 (g/cm3) | flame temp k (K) | fuel | hazard class | isp vac max s (s) | isp vac min s (s) | isp vac s (s) | metal content pct (%) | oxidizer | propellant type | source method |
|---|---|---|---|---|---|---|---|---|---|---|---|
| solid db ap hmx al | 1.8 | 4,000 | NC NG AP HMX Al binder | 1.1 | 270 | 265 | 267.5 | 20 | AP HMX integral | solid cmdb | CMDB with AP/HMX/Al. Solvent cast. Isp range 265-270 s. Density SG=1.80 (0.065 lbm/in3). Flame temp 4000 K. Metal content 20% Al. Pressure exponent n=0.49. Burning rate 0.2-1.2 in/s. |
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