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Rocket Propellant Properties: solid ctpb 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 ctpb ap al | 1.78 | 3,440 | CTPB binder Al | 1.3 | 265 | 260 | 262.5 | 16 | AP integral | solid composite | Composite: CTPB binder / AP / Al. Cast. Isp range 260-265 s. Density SG=1.78 (0.064 lbm/in3). Flame temp 3440 K. Metal content 15-17% Al. Pressure exponent n=0.40. Burning rate 0.25-2.0 in/s. |
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