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Atlas V 401

Atlas familyUnited Launch AllianceRetired

An Atlas V with a 4 meter diameter fairing, no boosters and a single centaur upper stage engine.

Atlas V 401 vehicle

Specifications

Thrust
3,827 kN
Height
58.3 m
Diameter
3.8 m
Launch mass
590 t
Stages
2
Launch cost
$115M
LEO capacity
9,050 kg
GTO capacity
4,950 kg
SSO capacity
6,670 kg

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

41flightswith a definitive outcome
100%success rate41 of 41
41success streakcurrent

Counted from padside's own launch record, the same basis as the stats page.

Flights

5 of 41

All 41 flights