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SRM-2
IUS
Credit: NASA
CSD solid rocket engine. Used in Shuttle, Titan 34D; IUS-2. Known by manufacturer as Orbus 6. First flight 1982.
AKA: IUS-2;Orbus 6. Status: Retired 2004. Number: 58 . Thrust: 78.40 kN (17,625 lbf). Gross mass: 3,919 kg (8,639 lb). Unfuelled mass: 1,170 kg (2,570 lb). Specific impulse: 304 s. Specific impulse sea level: 200 s. Burn time: 103 s. Height: 2.08 m (6.82 ft). Diameter: 1.61 m (5.28 ft).
Thrust (sl): 51.600 kN (11,600 lbf). Thrust (sl): 5,261 kgf.
Country:
USA.
Launch Vehicles:
Titan 34D/IUS,
Titan 34D,
Titan 402A/IUS,
Commercial Titan 3,
Titan 405A,
Titan 402B/IUS.
Propellants:
Solid.
Stages:
SRM-2.
Agency:
CSD.
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