Solid Rocket Booster  
Initial Operational Capability (IOC): 1981
Total Production: ?
Also Known As: SRB
Origin: United States of America
Parent System: Solid Rocket Booster
Initial Operational Capability (IOC): 1981
Total Production: ?
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Description: The Solid Rocket Booster (SRB) has been designed to assist heavy rockets and the Space Shuttle providing enough thrust during the liftoff. In 2011, the NASA announced that will use solid rocket boosters for the initial development flights of the Space Launch System (SLS), while follow-on boosters will be competed based on performance requirements and affordability considerations.

Solid Rocket Booster Applications

Space Systems Ares I Ares V SLS Evolved Lift Capability SLS Initial Lift Capability Space Shuttle

Solid Rocket Booster Specifications

Fuel Consumption
Average Fuel Weight Consumption: 5 ton/sec
Burn Time: 2 minute (120 second)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

Solid Rocket Booster News

There is 1 news
on 14 Sep 2011
Wednesday, September 14, 2011NASA Announces Design for SLS Deep Space Exploration System

Operators & Related Equipment


Grand Total ?1
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