Salman (rocket motor)
Rocket engine developed by Iran / From Wikipedia, the free encyclopedia
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The Salman (Persian: سلمان) is a solid-propellant rocket motor designed and built by the Islamic Revolutionary Guard Corps.[1][2] It is used as the second stage of the Qased and Qaem-100 satellite launch vehicles.[1][3] The system was announced on 9 February 2020[4] and was launched for the first time on 22 April 2020, placing Iran's first military satellite, named Noor, into orbit.[1][5]
Quick Facts Manufacturer, Country of origin ...
Manufacturer | IRGCASF |
---|---|
Country of origin | Iran |
Used on | Qased Qaem-100 |
General characteristics | |
Diameter | 1 m (3 ft 3 in) |
Gross mass | 1,900 kg (4,200 lb) |
Associated stages | |
Comparable | Star 48 , Castor 30 |
Launch history | |
Status | Active |
Total launches | 5 |
Successes (stage only) | 5 |
Failed | 0 |
First flight | 22 April 2020 |
Salman upper-stage | |
Burn time | 60 seconds |
Propellant | Solid |
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