by auroradude » Sun Mar 16, 2008 5:28 pm
The main engines (liquid hydrogen and liquid oxygen) account for only 17% of the thrust at liftoff. The other 83% is provided by the solid rocket boosters. Each external booster contains 1,100,000 pounds of propellent.
The propellant mixture in each SRB motor consists of ammonium perchlorate (oxidizer, 69.6% by weight), aluminum (fuel, 16%), iron oxide (a catalyst, 0.4%), a polymer (such as PBAN or HTPB, a binder that holds the mixture together, also acting as secondary fuel, 12.04%), and an epoxy curing agent (1.96%). This propellant is commonly referred to as Ammonium Perchlorate Composite Propellant, or simply APCP.
It's over two million pounds of a little more than just water but it sure looks cool when it burns!
The main engines (liquid hydrogen and liquid oxygen) account for only 17% of the thrust at liftoff. The other 83% is provided by the solid rocket boosters. Each external booster contains 1,100,000 pounds of propellent.
The propellant mixture in each SRB motor consists of ammonium perchlorate (oxidizer, 69.6% by weight), aluminum (fuel, 16%), iron oxide (a catalyst, 0.4%), a polymer (such as PBAN or HTPB, a binder that holds the mixture together, also acting as secondary fuel, 12.04%), and an epoxy curing agent (1.96%). This propellant is commonly referred to as Ammonium Perchlorate Composite Propellant, or simply APCP.
It's over two million pounds of a little more than just water but it sure [i]looks[/i] cool when it burns!