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.
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
0failuresincluding partial failures
41success streakcurrent
First flight August 21, 2002 · latest November 10, 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 401 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2002 | 1 | 0 | 1 |
| 2003 | 1 | 0 | 1 |
| 2004 | 0 | 0 | 0 |
| 2005 | 1 | 0 | 1 |
| 2006 | 0 | 0 | 0 |
| 2007 | 3 | 0 | 3 |
| 2008 | 0 | 0 | 0 |
| 2009 | 3 | 0 | 3 |
| 2010 | 1 | 0 | 1 |
| 2011 | 1 | 0 | 1 |
| 2012 | 3 | 0 | 3 |
| 2013 | 5 | 0 | 5 |
| 2014 | 7 | 0 | 7 |
| 2015 | 4 | 0 | 4 |
| 2016 | 3 | 0 | 3 |
| 2017 | 4 | 0 | 4 |
| 2018 | 1 | 0 | 1 |
| 2019 | 0 | 0 | 0 |
| 2020 | 0 | 0 | 0 |
| 2021 | 2 | 0 | 2 |
| 2022 | 1 | 0 | 1 |