Manufacturer TsSKB-Progress | Country of origin Russia | |
Diameter 2.72 metres (8 ft 11 in) Length 2.59 metres (8 ft 6 in) Gross mass 3,210 kilograms (7,080 lb) Empty mass 2,310 kilograms (5,090 lb) | ||
The Ikar was a rocket upper stage designed in Russia in 1999 to be used with the Soyuz 11A511U rocket as Soyuz-Ikar. It was derived from the propulsion module of the Yantar spy satellites.
References
Ikar (rocket stage) Wikipedia(Text) CC BY-SA