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Solid rocket booster

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Title: Solid rocket booster  
Author: World Heritage Encyclopedia
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Subject: Ariane 6, Comparison of orbital rocket engines, Liquid fly-back booster, STS-51-L Mission timeline, Booster (rocketry)
Collection: Rocketry, Solid-Fuel Rockets
Publisher: World Heritage Encyclopedia

Solid rocket booster

NASA Image of a solid rocket booster (right) being mated to a Delta II rocket (blue). Two boosters (white) can be seen already attached.

Solid rocket boosters (SRB), or solid rocket motors (SRM), are used to provide thrust in spacecraft launches from the launchpad up to burnout of the SRBs. Many launch vehicles include SRBs, including the Ariane 5, Atlas V (optional for extra thrust),[1] and the NASA Space Shuttle. The NASA Space Shuttle used two Space Shuttle SRBs, which were the largest of their type in production service. The propellant for each solid rocket motor on the Space Shuttle weighed approximately 500 000 kg.[2]

Compared to liquid-fuel rockets, the solid-fuel SRBs are advantageous for the purpose of boosting launches because they provide greater thrust and do not have the refrigeration and insulation requirements of liquid-fueled rockets. Adding detachable SRBs to a vehicle also powered by liquid-fueled rockets (known as staging) reduces the amount of liquid fuel needed and lowers the launch vehicle mass.

One example of the increased performance from SRBs is the Ariane 4 rocket. The basic 40 model with no boosters could lift a 2175 kilogram payload to Geostationary transfer orbit.[3] The 44P model with 4 solid boosters has a payload of 3465 kg to the same orbit.[4]

Solid boosters are usually cheaper to design, test, and produce compared to equivalent thrust liquid boosters. However, SRB costs on a per-flight basis tend to be equivalent to those of their liquid counterparts.

It is difficult to stop a solid rocket motor before normal burnout. This can be done by explosively separating the nozzle and/or splitting the case lengthwise with a linear shaped charge. The latter method is common in range safety destruct systems. Either method terminates thrust by reducing combustion chamber pressure and propellant burn rate, though the propellant (usually in many pieces at this point) will continue to burn vigorously.

SRB failure rates are about 1%. They usually fail in sudden, catastrophic explosions due to overpressurization, the SRB failure mode on Challenger being an exception.

Solid rocket motors also present a significant handling risk on the ground. Once their propellant is poured into place and cured, they can catch fire or explode. Such an accident occurred on August 22, 2003, killed 21 technicians at the Brazilian VLS rocket launch pad.[5] Liquid rocket boosters generally cannot be moved after tanking.

See also


 This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.

  1. ^ "Data", Assets ( .
  2. ^ "Solid rocket boosters". USA: NASA. 2009-08-09. .
  3. ^ Ariane 4, Astronautix .
  4. ^ Ariane 44P, Astronautix .
  5. ^ VLS

External links

  • HowStuffWorks : Sold Fuel Rocket Engines
  • NASA website about the solid rocket booster
  • U.S. Centennial of Flight Commission article on solid propelled rockets
  • NASA CGI video developed for the Ares program showing recovery of solid rocket booster
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