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Atlas V 501

Atlas familyUnited Launch AllianceRetired

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

Atlas V 501 vehicle

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

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

Flight record

8flightswith a definitive outcome
100%success rate8 of 8
0failuresincluding partial failures
8success streakcurrent

First flight April 22, 2010 · latest October 6, 2023 · 18:06 UTC

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 501 flights per year
Atlas V 501 flights per year
YearSuccessfulFailedTotal
2010202
2011101
2012101
2013101
2014000
2015101
2016000
2017000
2018000
2019000
2020101
2021000
2022000
2023101

Flights

5 of 8

All 8 flights