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Viking 4

Viking 4 is Snecma Moteurs’ storable-propellant liquid rocket engine for the Ariane second stage. ESA’s Ariane 4 reference identifies a single Viking 4 using nitrogen tetroxide and UH25, with 798 kN engine thrust and a 125-second stage firing. That upper-stage figure describes the named Ariane 4 installation; it should be read separately from the first-stage Viking 5 and liquid-booster Viking 6 ratings. The Ariane 4 vehicle family completed service in 2003.

Identity

Aliases
Viking 4Viking-4Snecma Viking 4Ariane second-stage Viking 4
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
Viking 4
Status
retired

Details

Description
Viking 4 is Snecma Moteurs’ storable-propellant liquid rocket engine for the Ariane second stage. ESA’s Ariane 4 reference identifies a single Viking 4 using nitrogen tetroxide and UH25, with 798 kN engine thrust and a 125-second stage firing. That upper-stage figure describes the named Ariane 4 installation; it should be read separately from the first-stage Viking 5 and liquid-booster Viking 6 ratings. The Ariane 4 vehicle family completed service in 2003.
First Flight Date
1979-12-24
Propellants
nitrogen tetroxideUH25
Rocket Specs
Burn Time
…

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Creation Time
August 1, 2026 at 08:31:02 UTC
Updated Time
October 29, 2026 at 15:26:36 UTC

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