ATLAS V N22 V N22
EXPENDABLE 2-STAGE LAUNCH VEHICLE
ACTIVE
Technical Overview
Length
height
58
m
Diameter
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3.8
m
Payload to LEO
rocket
13,034
kg
Engine Details
RD-180
RD-180 is the dual-chamber kerolox main engine used on Atlas V first stages.
Propellant
LOX / RP-1
Thrust
860,000 lbf
Cycle
Staged combustion
Flight History
*Since 2019-12-20
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Total Launches
3
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3 consecutive successes
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Successful Launches
3
verified
100% success rate
warning
Failed Launches
0
schedule
6 pending