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SRB Stats
Thrust at lift-off:
2,650,000 pounds
Propellant Properties:
16% Atomized aluminum powder (fuel)
69.8% Ammonium perchlorate (oxidizer)
.2% Iron oxide powder (catalyst )
12% Polybutadiene acrylic acid acrylonite (binder)
2% Epoxy curing agent
Weight
Empty: 193,000 pounds
Propellant:
1,107,000 pounds
Gross: 1,300,000 pounds
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+ More NASA Facts...
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| |  | | | | Solid Rocket Boosters
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The Solid Rocket Boosters (SRBs) operate in parallel with the main engines for the first two minutes of flight to provide the additional thrust needed for the Orbiter to escape the gravitational pull of the Earth. At an altitude of approximately 45 km (24 nautical miles), the boosters separate from the orbiter/external tank, descend on parachutes, and land in the Atlantic Ocean (+ View Video: SRB Processing). They are recovered by ships, returned to land, and refurbished for reuse. The boosters also assist in guiding the entire vehicle during initial ascent. Thrust of both boosters is equal to 5,300,000 lbs.
Image left: The Solid Rocket Boosters separate from the Shuttle about two minutes after launch Click image to play video of SRB separation (no audio) Photo credit: NASA.
In addition to the solid rocket motor, the booster contains the structural, thrust vector control, separation, recovery, and electrical and instrumentation subsystems. ( + View Diagram )
The solid rocket motor is the largest solid propellant motor ever developed for space flight and the first built to be used on a manned craft. The huge motor is composed of a segmented motor case loaded with solid propellants, an ignition system, a movable nozzle and the necessary instrumentation and integration hardware.
 Image to right: In a Vehicle Assembly Building high bay, an aft center segment of a Solid Rocket Booster is lowered toward a segment already in place. Credit: NASA
Each solid rocket motor contains more than 450,000 kg (1,000,000 lb.) of propellant, which requires an extensive mixing and casting operation at a plant in Utah. The propellant is mixed in 600 gallon bowls located in three different mixer buildings. The propellant is then taken to special casting buildings and poured into the casting segments.
Cured propellant looks and feels like a hard rubber typewriter eraser. The combined polymer and its curing agent is a synthetic rubber. Flexibility of the propellant is controlled by the ratio of binder to curing agent and the solid ingredients, namely oxidizer and aluminum. The solid fuel is actually powdered aluminum -- a form similar to the foil wraps in your kitchen -- mixed with oxygen provided by a chemical called ammonium perchlorate.
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