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Rocket Motor
Propellants
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Double Base
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Double-base propellants are mainly composed of nitrocellulose
and nitroglycerine. Additives are included to control ballistic and mechanical
properties and to ensure chemical stability
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Double-base propellants can be extruded in an extrusion
press or cast in a mould
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Performance
- Ispec: 2200 - 2400 m/s
- Tc: 2300 - 2800 K
- Density: 1.60 - 1.65 x 103 kg/m3
- operational temperature -40°C - +65°C
- non corrosive combustion gases
- minimum smoke
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