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Rocket Propellant Properties: solid db ap 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 al | 1.8 | 3,880 | NC NG AP Al binder | 1.3 | 265 | 260 | 262.5 | 20 | AP integral | solid cmdb | Composite-modified double base (CMDB/DB-AP-Al). Extruded. Isp range 260-265 s. Density SG=1.80 (0.065 lbm/in3). Flame temp 3880 K. Metal content 20-21% Al. Pressure exponent n=0.40. Burning rate 0.2-1.0 in/s. |
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