AESTUS

Launch Vehicle Engine by ArianeGroup (4 more products)

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The AESTUS from ArianeGroup is a Launch Vehicle Engine with Engine Mass 111 Kg (Chamber), Nozzle Outlet Diameter 1.31 m, Propellant Flow Rate 9.3 Kg/s, Specific Impulse 324 sec, Vacuum Thrust 29.6 kN. More details for AESTUS can be seen below.

Product Specifications

Product Details

  • Part Number
    AESTUS
  • Manufacturer
    ArianeGroup
  • Description
    The Aestus engine powers the Ariane 5 ES version bipropellant upper stage for insertion of payloads into LEO, SSO and GTO.

General Parameters

  • Engine Mass
    111 Kg (Chamber)
  • Nozzle Outlet Diameter
    1.31 m
  • Propellant
    N2O4, MMH
  • Propellant Flow Rate
    9.3 Kg/s
  • Specific Impulse
    324 sec
  • Vacuum Thrust
    29.6 kN

Technical Documents