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Soyuz-FG
EntityQ2415633· pop 21· linked from 475 articles

The Soyuz-FG was an improved variant of the Soyuz-U launch vehicle from the R-7 rocket family, developed by the Progress Rocket Space Centre in Samara, Russia. It featured upgraded first and second stage engines, RD-107A and RD-108A, respectively, with enhanced injector heads that improved combustion efficiency and specific impulse. The designation "FG" refers to forsunochnaya golovka (injector head) in Russian.

Key facts

Rocket.name
Soyuz-FG
Rocket.image
Soyuz TMA-3 launch.jpg
Rocket.caption
The launch of Soyuz TMA-3 atop a Soyuz-FG rocket.
Rocket.function
Medium-lift launch vehicle
Rocket.manufacturer
RKTs Progress
Rocket.country origin
Russia
Rocket.cpl
(2012)
Rocket.family
R-7 (Soyuz)
Rocket.derived_from
Soyuz-U
Rocket.derivatives
Soyuz-2
Rocket.status
Retired
Rocket.sites
Baikonur, LC-1/5 and LC-31/6
Rocket.success
69
Rocket.fail
1 (Soyuz MS-10)
Rocket.first
20 May 2001 (Progress M1-6)
Rocket.last
25 September 2019 (Soyuz MS-15)
Rocket/payload.location
LEO
Rocket/payload.inclination
51.8°

via Wikipedia infobox

~13 min read

Encyclopedic overview

6 sections
Contents
  • Design
  • Launch history
  • See also
  • Notes
  • References
  • External links

The Soyuz-FG was an improved variant of the Soyuz-U launch vehicle from the R-7 rocket family, developed by the Progress Rocket Space Centre in Samara, Russia. It featured upgraded first and second stage engines, RD-107A and RD-108A, respectively, with enhanced injector heads that improved combustion efficiency and specific impulse. The designation "FG" refers to forsunochnaya golovka (injector head) in Russian.

Soyuz-FG made its maiden flight on 20 May 2001, delivering a Progress cargo spacecraft to the International Space Station (ISS). It became the primary vehicle for launching crewed Soyuz TMA, Soyuz TMA-M, and Soyuz MS spacecraft from 2002 until its retirement in 2019.

Excerpted from Wikipedia’s “Soyuz-FG” article, available under the CC BY-SA 4.0 licence.