| | Parameter | Value |
| | Propellant grain length, | 52 cm | | Initial port diameter, | 3.6 cm | | Nozzle throat diameter, | 1.6 cm | | Grain/nozzle-conv. length ratio, | 16 : 1 | | Propellant specific heat, | 1500 J/kg-K | | Propellant density, | 1730 kg/m3 | | Propellant thermal conductivity, | 0.4 W/m-K | | Propellant thermal diffusivity, | 1.54 × 10-7 m2/s | | Propellant flame temperature, | 3000 K | | Propellant surface temperature, | 1000 K | | Propellant initial temperature, | 294 K | | Gas specific heat, | 1920 J/kg-K | | Specific gas constant, | 320 J/kg-K | | Gas thermal conductivity, | 0.2 W/m-K | | Gas absolute viscosity, μ | 8.07 × 10-5 kg/m-s | | Gas specific heat ratio, γ | 1.2 | | De St. Robert exponent, | 0.35 | | De St. Robert coefficient, | 0.05 cm/s-(kPa)n | | Particle solid density, | 2700 kg/m3 | | Particle specific heat, J/kg-K | 900 J/kg-K | | Particle mass fraction, | 0% | | Propellant elastic modulus, | 45 MPa | | Propellant Poisson’s ratio, | 0.497 | | Casing inner wall radius, | 3.24 cm | | Casing wall thickness, | 0.127 cm | | Casing material density, | 2700 kg/m3 | | Casing elastic modulus, | 80 GPa | | Casing material Poisson’s ratio, | 0.33 | | Sleeve wall thickness, | 0.47 cm | | Sleeve material density, | 7850 kg/m3 | | Sleeve elastic modulus, | 200 GPa | | Sleeve material Poisson’s ratio, | 0.30 | | Casing/prop. rad. damping ratio, | 0.35 | | Casing/prop. long. damping ratio, | 0.10 |
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