| 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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