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Geschreven door Tony Vyverman
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zondag, 30 september 2007 |
Could you tell me the relation between burning rate and pressure for Zn/S propellant ?
Is there any equation like r = bP^n that is possible to be considered for this type of fuel ?
If I know burning surface and throat diameter how can I determine pressure?
Can I use the same equations as I use for other solid rocket fuels ?
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Gewijzigd op ( zondag, 30 september 2007 )
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