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SOYUZ-FG Launch Vehicle
"Soyuz-FG" launch vehicle is intended for injection of automatic spacecraft for national economy, scientific research ("Resurs-F1", "Resurs-F2", "Foton" spacecraft) and spacecraft for special purposes ("Kosmos"-series satellites) as well as manned and cargo spaceships according to the program of the International Space Station.
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SOYUZ-FG Launch Vehicle
"Soyuz-FG" launch vehicle is intended for injection of automatic spacecraft for national economy, scientific research ("Resurs-F1", "Resurs-F2", "Foton" spacecraft) and spacecraft for special purposes ("Kosmos"-series satellites) as well as manned and cargo spaceships according to the program of the International Space Station.
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SOYUZ-FG Launch Vehicle
"Soyuz-FG" launch vehicle is intended for injection of automatic spacecraft for national economy, scientific research ("Resurs-F1", "Resurs-F2", "Foton" spacecraft) and spacecraft for special purposes ("Kosmos"-series satellites) as well as manned and cargo spaceships according to the program of the International Space Station.
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SOYUZ-FG Launch Vehicle
"Soyuz-FG" launch vehicle is intended for injection of automatic spacecraft for national economy, scientific research ("Resurs-F1", "Resurs-F2", "Foton" spacecraft) and spacecraft for special purposes ("Kosmos"-series satellites) as well as manned and cargo spaceships according to the program of the International Space Station.
SOYUZ-FG Launch Vehicle
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"Soyuz-FG" launch vehicle is intended for injection of automatic spacecraft for national economy, scientific research ("Resurs-F1", "Resurs-F2", "Foton" spacecraft) and spacecraft for special purposes ("Kosmos"-series satellites) as well as manned and cargo spaceships according to the program of the International Space Station.
In contrast to "Soyuz-U" launch vehicle modernized engines with heightened specific thrust on units of the 1-st and the 2-nd stages, developed for "Soyuz-2" launch vehicle, are used for "Soyuz-FG" launch vehicle for increasing load-carrying capacity.
"Soyuz-FG" launch vehicle can be equipped with nose fairing of the following diameter: 3,0 m. The confirmed serviceability index of "Soyuz-FG" launch vehicle - 0, 985. |
SOYUZ-FG Launch Vehicle
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Capabilities of Soyuz-FG (when launched with a nose fairing of ø 3.0 m)
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