Padside

Atlas V 501

Atlas family · United Launch Alliance · Retired

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Atlas V with 5m Fairing, 0 SRB, 1 Centaur upper stage engine.

Specifications

Thrust
3,827 kN
Height
58.3 m
Diameter
3.8 m
Launch mass
334 t
Stages
2
Launch cost
$120M
LEO capacity
8,210 kg
GTO capacity
3,780 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
8
Launches with a definitive outcome
Success rate
100%
8 of 8
Current success streak
8
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