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Atlas V 541

Atlas familyUnited Launch AllianceRetired

Atlas V with 5m Fairing, 4 SRB, 1 Centaur upper stage engine.

Atlas V 541 vehicle

Specifications

Thrust
10,581 kN
Height
60 m
Diameter
3.8 m
Launch mass
479 t
Stages
2
Launch cost
$145M
LEO capacity
17,410 kg
GTO capacity
8,290 kg
GEO capacity
3,530 kg

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

Flight record

9flightswith a definitive outcome
100%success rate9 of 9
0failuresincluding partial failures
9success streakcurrent

First flight November 26, 2011 · 15:02 UTC · latest July 1, 2022

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

Flights per year

  • Successful
  • Failed
Show the numbers for Atlas V 541 flights per year
Atlas V 541 flights per year
YearSuccessfulFailedTotal
2011101
2012000
2013000
2014202
2015000
2016101
2017101
2018101
2019000
2020101
2021000
2022202

Flights

5 of 9

All 9 flights