ANGARA 1.2 1.2
EXPENDABLE 2-STAGE LAUNCH VEHICLE
ACTIVE
Technical Overview
Length
height
41.5
m
Diameter
radio_button_unchecked
2.9
m
Launch Mass
scale
171
t
Payload to LEO
rocket
3,700
kg
Payload to SSO
satellite_alt
2,400
kg
Engine Details
RD-191
RD-191 is the single-chamber kerolox engine used on the Angara 1.2 core stage.
Propellant
LOX / RP-1
Thrust
1,922 kN
Cycle
Oxygen-rich staged combustion
Flight History
*Since 2014-07-09
rocket_launch
Total Launches
6
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6 consecutive successes
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Successful Launches
6
verified
100% success rate
warning
Failed Launches
0
schedule
Recorded failures