Sample data from Engineering Database — 375 reference tables, deterministic calculators, and Engineering AI. Sign up free
Rocket Propellant Properties: solid an polymer
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 an polymer | 1.47 | 1,550 | polymer binder | 1.3 | 190 | 180 | 185 | 0 | AN integral | solid gas generator | Composite: Ammonium Nitrate (AN) / Polymer binder. Gas generator propellant. Isp range 180-190 s. Density SG=1.47 (0.053 lbm/in3). Flame temp 1550 K. Zero metal content. Pressure exponent n=0.60. Burning rate 0.06-0.5 in/s. Smokeless clean exhaust; low performance. |
What else is in Engineering Database
Iron Engine ↗Engineering AI at ironengine.ai
AI built for engineering. Searches the engineering database, performs calculations, gives source-backed engineering insights.
Get started for free ↗Reference Data375 engineering tablesMaterial properties, pipe and shape dimensions, code tables, and electrical ratings across mechanical, civil, chemical, electrical, materials, and manufacturing engineering.
Browse dataCalculatorsDeterministic engineering calculatorsSizing, checking, and conversion tools that run against the reference tables. Inputs are code-compliant, outputs are traceable to the source standard.
Browse calculators