Atlas family
Atlas V 431
Atlas V with 4m Fairing, 3 SRB, 1 Centaur upper stage engine.
Flights flown3
Success rate100%3/3
Payload to LEO15,260kg
Cost per kg to LEO$8,519$130M per launch
Maiden flight2005-03-11
Peak year20051 flight
Atlas V 431 is built by United Launch Alliance of the United States. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 11 March 2005 and last flew on 18 December 2016.
Flight record
100% success rate3 of 3 flown
2005peak 2005 · 1 flight2016
First flight2005-03-11
Latest flight2016-12-18
Failures0
Consecutive successes3
Fastest turnaround1717d 9h
Payload
| Low Earth orbit | 15,260kg |
|---|---|
| Geostationary transfer orbit | 7,700kg |
| Geostationary orbit | 2,820kg |
| Launch cost | $130M |
| Cost per kg to LEO | $8,519 |
Vehicle
| Stages | 2 |
|---|---|
| Length | 59.1m |
| Diameter | 3.8m |
| Launch mass | 479t |
| Maiden flight | 2005-03-11 |
| Reusable | No |
Pads used
Orbits delivered
Geostationary Transfer Orbit2Geosynchronous Transfer Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 2016-12-18 | Atlas V 431 | Echostar 19 (Jupiter-2) | Space Launch Complex 41 | Geostationary Transfer Orbit | Success |
| 2009-11-23 | Atlas V 431 | Intelsat 14 | Space Launch Complex 41 | Geostationary Transfer Orbit | Success |
| 2005-03-11 | Atlas V 431 | INMARSAT 4 F1 | Space Launch Complex 41 | Geosynchronous Transfer Orbit | Success |
Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.