Padside

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Start family · Moscow Institute of Thermal Technology · Retired

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Russian orbital launch vehicle. Launch vehicle based on decommissioned SS-25 ICBM's launched from mobile transporter.

Specifications

Thrust
887 kN
Height
28.9 m
Diameter
1.61 m
Launch mass
60 t
Stages
5
Launch cost
$10.5M
LEO capacity
645 kg
GTO capacity
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
1
Launches with a definitive outcome
Success rate
0%
0 of 1
Current success streak
0
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
Between consecutive booster flights

Counted from padside's own launch record — the same basis as the Stats page.

Launches