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Angara Stage 2

Stage · Russia

Original archive entry. The text, images and links below are kept as they were written.

LOx/LH2 propellant rocket stage. Unique configuration with oxidizer in core and fuel in two tanks strapped on in parallel - all of rail-transportable 3.9 m diameter. Built by NPO Energia to Khrunichev design (their own design for Angara and Energia-M were rejected in favor of Khrunichev version). Masses estimated based on engine selected and vehicle performance. Assumed that engine is throttled back to maintain constant 3-G acceleration.

Country
Russia
Engines
RD-0120M
Propellants
Lox/LH2