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Rocket Propellant Properties: solid db
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 | 1.61 | 2,550 | NC NG binder | 1.1 | 230 | 220 | 225 | 0 | none premixed solid | solid db | Double base solid propellant (extruded). NC binder plasticized with NG. Isp range 220-230 s. Density SG=1.61 (0.058 lbm/in3). Flame temp 2550 K. Smokeless; zero metal content. Pressure exponent n=0.30. Burning rate 0.05-1.2 in/s. Mechanical: stress/strain at -60F: 4600 psi/2%; at +150F: 490 psi/60%. |
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