For an assignment, I am to find the stoichiometric values for a few different reactants in solid rocket mixtures. for fuel, I am using pure crystalline aluminum and HTPB (C654H988N8O20). for an oxidizer, I am using ammonium nitrate (NH4NO3). I'm not sure how to predict the products of this reaction. can anyone help?
Al + NH4NO3 + C654H988N8O20 = ?
Thanks!
products of a solid rocket propellant reaction
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