H3-30 30
EXPENDABLE 2-STAGE LAUNCH VEHICLE
ACTIVE
Technical Overview
Length
height
63
m
Diameter
radio_button_unchecked
5.3
m
Launch Mass
scale
274
t
Payload to GTO
public
2,300
kg
Payload to SSO
satellite_alt
4,000
kg
Engine Details
LE-9
H3-30 uses the LE-9 hydrolox first-stage engine family and LE-5B-3 on the upper stage.
Propellant
LOX / LH2
Thrust
1,471 kN (sea level)
Upper Stage
LE-5B-3
Flight History
*Current Launch Library totals
rocket_launch
Total Launches
0
trending_up
Tracked launch count
check_circle
Successful Launches
0
verified
Completed launches
warning
Failed Launches
0
schedule
1 pending