Soyuz (Rocket)

1966
OKB-1 Soyuz (Rocket) 1966 - Hero viewOKB-1 Soyuz (Rocket) 1966 - Capsule viewOKB-1 Soyuz (Rocket) 1966 - Fairing viewOKB-1 Soyuz (Rocket) 1966 - Instruments view
Hero
Most launched

The most-launched rocket family in history with over 1,900 flights. Descended from Korolev''s R-7, the same design that launched Sputnik. For nearly a decade after the Shuttle retired, Soyuz was the only vehicle carrying astronauts to the International Space Station.

History

The Soyuz rocket is a direct descendant of the R-7, designed by Sergei Korolev as the Soviet Union''s first intercontinental ballistic missile. The R-7 launched Sputnik in 1957 and Yuri Gagarin in 1961, and its basic design -- a central core surrounded by four tapered boosters -- has been in continuous use for over sixty years.

The Soyuz variant emerged in the mid-1960s as a dedicated space launch vehicle, optimized for carrying the Soyuz crewed spacecraft to orbit. Over the decades, the rocket was progressively upgraded while maintaining its fundamental architecture. The current Soyuz-2 version uses digital flight computers and improved engines, but a pilot from the 1960s would still recognize the vehicle instantly.

After the Space Shuttle''s retirement in 2011, Soyuz became the sole means of transporting crew to the International Space Station, a role it held until SpaceX''s Crew Dragon began flying in 2020. During that period, NASA paid Roscosmos approximately $80 million per seat to fly astronauts on Soyuz -- a testament to both the vehicle''s reliability and the lack of alternatives.

With over 1,900 launches across the entire R-7/Soyuz family, no other rocket design comes close in total missions flown. The vehicle''s longevity is a testament to the soundness of Korolev''s original design and the Russian engineering philosophy of incremental improvement over radical innovation.

Timeline

1957The R-7 launched Sputnik in 1957 and Yuri Gagarin in 1961
1966First flight
2011After the Space Shuttle''s retirement in 2011

Production & Heritage

DesignerSergei Korolev
Service Period1966

Technical Specifications

PropulsionLiquid (RP-1/LOX)
Height151.9 ft
Length151.9 ft
Diameter/Wingspan9.7 ft
Crew3
Gross Mass687,841 lbs

Propulsion

Engine ModelRD-108A (core) / RD-107A (boosters) / RD-0110 (Block I)
Engine Count5
Engine ManufacturerNPO Energomash / KB Khimmash
Thrust932,000 lbf
Specific Impulse311 s
PropellantRP-1 / LOX
Stages3
Boosters4

Performance

Max Speed28,800 km/h
Payload to LEO7,020 kg
Payload to GTO3,250 kg

Dimensions

Height (m)46.3 m
Diameter (m)10.3 m
Length (m)46.3 m

Mass

Empty Mass (kg)24,000 kg
Gross Mass (kg)312,000 kg

Mission

Mission Duration1900+ launches since 1966, most-used crewed launch vehicle
Missions Flown1980
Success Rate1920/1980
ReusableNo

Power & Systems

AvionicsDigital flight computer (modern variants), evolved from R-7 guidance
Communication BandS-band, VHF telemetry

Tags

Designed by Sergei Korolev

Featured in

Featured in Collections

Keep Exploring

View all vehicles
Space HeritageCookie Preferences

We use only essential cookies to make this archive work. No tracking or advertising cookies.

Learn more