Atlas V 431
Atlas familyUnited Launch AllianceRetired
Atlas V with 4m Fairing, 3 SRB, 1 Centaur upper stage engine.
Specifications
- Thrust
- 8,892 kN
- Height
- 59.1 m
- Diameter
- 3.8 m
- Launch mass
- 479 t
- Stages
- 2
- Launch cost
- $130M
- LEO capacity
- 15,260 kg
- GTO capacity
- 7,700 kg
- GEO capacity
- 2,820 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
100%success rate3 of 3
0failuresincluding partial failures
3success streakcurrent
First flight March 11, 2005 · latest December 18, 2016
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 431 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2005 | 1 | 0 | 1 |
| 2006 | 0 | 0 | 0 |
| 2007 | 0 | 0 | 0 |
| 2008 | 0 | 0 | 0 |
| 2009 | 1 | 0 | 1 |
| 2010 | 0 | 0 | 0 |
| 2011 | 0 | 0 | 0 |
| 2012 | 0 | 0 | 0 |
| 2013 | 0 | 0 | 0 |
| 2014 | 0 | 0 | 0 |
| 2015 | 0 | 0 | 0 |
| 2016 | 1 | 0 | 1 |