The primary propellants were ammonium perchlorate (oxidizer) and atomized aluminum powder (fuel), and the total propellant for each solid rocket motor weighed approximately 1,100,000 lb (500 t) (see § Propellant). The inert weight of each SRB was approximately 200,000 pounds (91 t).
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Answer:
powdered aluminum -- a form similar to the foil wraps in your kitchen -- mixed with oxygen provided by a chemical called ammonium perchlorate
Answer:
The primary propellants were ammonium perchlorate (oxidizer) and atomized aluminum powder (fuel), and the total propellant for each solid rocket motor weighed approximately 1,100,000 lb (500 t) (see § Propellant). The inert weight of each SRB was approximately 200,000 pounds (91 t).
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