Solid Rocket Booster

Solid-fuel rocket boosters (SRBs) are large solid propellant motors used to provide thrust in spacecraft launches from initial launch through the first ascent stage. Many launch vehicles, including the Ariane 5, Atlas V, and the NASA Space Shuttle, have used SRBs to give launch vehicles much of the thrust required to escape Earth's gravitational pull. The Space Shuttle Solid Rocket Boosters were the largest solid propellant motors ever built and designed for recovery and reuse.

Solid-fuel rocket boosters (SRBs) are large solid propellant motors used to provide thrust in spacecraft launches from initial launch through the first ascent stage. Many launch vehicles, including the Ariane 5, Atlas V, and the NASA Space Shuttle, have used SRBs to give launch vehicles much of the thrust required to escape Earth's gravitational pull. The NASA Space Shuttle used two Space Shuttle SRBs, which were the largest solid propellant motors ever built and the first designed for recovery and reuse. The propellant for each solid rocket motor on the Space Shuttle weighed approximately 500,000 kilograms.

Compared to liquid propellant rockets, the solid-propellant SRBs have been capable of providing large amounts of thrust with a relatively simple design. They provide greater thrust without significant refrigeration and insulation requirements. Adding detachable SRBs to a vehicle also powered by liquid-propelled rockets known as staging reduces the amount of liquid propellant needed and lowers the launch vehicle mass. Solid boosters have usually been cheaper to design, test, and produce in the long run compared to the equivalent liquid propellant boosters. Reusability of components across multiple flights, as in the Shuttle assembly, also has decreased hardware costs. However, SRB costs on a per-flight basis tend to be equivalent to those of their liquid counterparts.

One example of increased performance provided by SRBs is the Ariane 4 rocket. The basic 40 model with no additional boosters was capable of lifting a 2,175 kilogram payload to Geostationary transfer orbit. The 44P model with 4 solid boosters has a payload of 3,465 kg to the same orbit.

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