Auto Credit Based on simpleaerospace's USSR/Russia/Ukraine Zenit 2

The booster would use engines developed for the Zenit. The first Angara design by Khrunichev featured a unique parallel fuel tank configuration in both first and second stages. This concept beat two competing NPO Energia designs: the Energia-M and a 'clean sheet' in-line concept. However the second stage was initially subcontracted to Energia by Khrunichev.

From : Astronautix

GENERAL INFO

PERFORMANCE

  • Total Delta V: 6.7km/s
  • Total Thrust: 34.2MN
  • Engines: 26
  • Wet Mass: 9.41E+5kg
  • Dry Mass: -1,130kg

STAGES

Stage Engines Delta V Thrust Burn Mass
1 4 3.7km/s 19.1MN 1.7m 9.41E+5kg
2 0 0m/s 0N 0s 8.73E+5kg
3 6 3.0km/s 9.8MN 73s 3.89E+5kg
4 0 0m/s 0N 0s 2.28E+5kg

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