Athena family
Athena II
The Athena II is an American small expendable launch system which was used for three launches between 1998 and 1999.
Flights flown3
Success rate66.7%2/3
Payload to LEO2,065kg
Maiden flight1998-01-07
Peak year19992 flights
Athena II is built by Lockheed Martin of the United States. Company background, funding, contracts and news for this operator are tracked on Space Index. It first flew on 7 January 1998 and last flew on 24 September 1999.
Flight record
66.7% success rate2 of 3 flown · 1 failed
1998peak 1999 · 2 flights1999
First flight1998-01-07
Latest flight1999-09-24
Failures1
Consecutive successes1
Fastest turnaround149d 23h
Payload
| Low Earth orbit | 2,065kg |
|---|---|
| Sun-synchronous orbit | 1,165kg |
| Geostationary transfer orbit | 593kg |
Vehicle
| Stages | 4 |
|---|---|
| Length | 28.2m |
| Diameter | 2.36m |
| Launch mass | 120t |
| Liftoff thrust | 1,900kN |
| Maiden flight | 1998-01-07 |
| Reusable | No |
Pads used
Orbits delivered
Polar Orbit2Lunar Orbit1
Launch history
| Date | Mission | Pad | Orbit | Outcome |
|---|---|---|---|---|
| 1999-09-24 | Athena II | Ikonos | Space Launch Complex 6 | Polar Orbit | Success |
| 1999-04-27 | Athena II | Ikonos 1 | Space Launch Complex 6 | Polar Orbit | Failure |
| 1998-01-07 | Athena II | Lunar Prospector | Space Launch Complex 46 | Lunar 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.
Further reading: Wikipedia