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Soyuz-7

Spacecraft and Launch Vehicles

Soyuz-7, also called Amur, is a Russian medium-lift orbital launch vehicle that exists only as a design concept. It is meant to be partially reusable and to burn liquid methane with liquid oxygen, which makes it a break from the kerosene-fuelled R-7 lineage behind every earlier Soyuz. The idea started at the Samara rocket maker now called the Progress Rocket Space Centre in the mid-2010s as a possible replacement for Soyuz-2, with a basic two-stage version planned for about nine tonnes to low Earth orbit and larger versions beyond it. By 2020 the concept had been reworked as Amur, and Roscosmos signed a contract for its preliminary design in October 2020. As described in 2020, Amur would stand about 55 metres tall and 4.1 metres across, lift off at about 360 tonnes, and fly from Vostochny with a reusable first stage using five RD-0169A engines. By late 2024 its first launch had slipped to around 2030, and a prototype first stage called Grasshopper was being considered.

Facts
Propulsion
Liquid Methane 1
Engine Class
Rocket 1
Status
Under development 1
Maximum Mass (kg)
360,000 1
Comparison
Body Style
Launch vehicle 1
Connections

Exemplifies

Source Soyuz-7 (Wikipedia)

Of Make

Source Soyuz-7 (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Soyuz-7 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
JSC SRC Progress originally proposed this new family of Russian rockets in the mid-2010s to replace the legacy Soyuz in the early 2020s.

Originated In

Also in Geography Atlas: where this subject originated.

Source Soyuz-7 (Wikipedia)Lead, country
Quote, Lead, country
currently in the design concept stage of development by the Roscosmos State Corporation in Russia
Sources
1. Soyuz-7 (Wikipedia)
  • Lead, status
    currently in the design concept stage of development by the Roscosmos State Corporation in Russia
  • History, 2013
    The proposed new design was to be based on a new propellant: LOX and liquid methane
  • History, 2015
    The methalox rocket was later renamed to Soyuz-7.
  • Lead, body style
    orbital launch vehicle currently in the design concept stage of development
  • Description, liftoff mass
    with a gross liftoff mass of 360 t (790,000 lb)
  • Lead, manufacturer
    JSC SRC Progress originally proposed this new family of Russian rockets in the mid-2010s to replace the legacy Soyuz in the early 2020s.
  • Lead, country
    currently in the design concept stage of development by the Roscosmos State Corporation in Russia
  • Of Make: Progress Rocket Space Centre, Lead
    JSC SRC Progress originally proposed this new family of Russian rockets in the mid-2010s to replace the legacy Soyuz in the early 2020s.
  • In Group: Orbital Launch Vehicles, Lead, vehicle type
    orbital launch vehicle currently in the design concept stage of development
  • Exemplifies: Orbital Spaceflight, Lead, mode
    orbital launch vehicle currently in the design concept stage of development
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