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Rocket Propellant Properties: solid pvc ap al

Rocket propellant performance data — specific impulse, characteristic velocity, chamber conditions for bipropellant, solid, and monopropellant combinations

Chemical Engineeringpropellant id: solid pvc ap al1 row
propellant iddensity g cm3 (g/cm3)flame temp k (K)fuelhazard classisp vac max s (s)isp vac min s (s)isp vac s (s)metal content pct (%)oxidizerpropellant typesource method
solid pvc ap al1.783,380PVC binder Al1.3265260262.521AP integralsolid compositeComposite: PVC binder / AP / Al. Cast or extruded. Isp range 260-265 s. Density SG=1.78 (0.064 lbm/in3). Flame temp 3380 K. Metal content 21% Al. Pressure exponent n=0.35. Burning rate 0.3-0.9 in/s.

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