Auto Credit Based on simpleaerospace's Angara (1995 design) (Alpha version)

Various alternative configurations of the Angara rocket were studied at Khrunichev including this heavy Angara-4E, which would combine hydrogen core stage with external tanks and four standard boosters burning kerosene. This particular configuration enabled to fire the hydrogen engine on the ground, thus simplfying the flight profile. Credit: GKNPTs Khrunichev.

GENERAL INFO

PERFORMANCE

  • Total Delta V: 9.4km/s
  • Total Thrust: 16.6MN
  • Engines: 25
  • Wet Mass: 4.44E+5kg
  • Dry Mass: 25,962kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 5 9.4km/s 9.9MN 3.7m 4.44E+5kg
2 0 0m/s 0N 0s 2.62E+5kg
3 0 0m/s 0N 0s 2.31E+5kg

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