Athena II
Athena familyLockheed MartinRetired
The Athena II is an American small expendable launch system which was used for three launches between 1998 and 1999.
Specifications
- Thrust
- 1,900 kN
- Height
- 28.2 m
- Diameter
- 2.36 m
- Launch mass
- 120 t
- Stages
- 4
- LEO capacity
- 2,065 kg
- GTO capacity
- 593 kg
- SSO capacity
- 1,165 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
66.7%success rate2 of 3
1failureincluding partial failures
1success streakcurrent
First flight January 7, 1998 · latest September 24, 1999
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Athena II flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1998 | 1 | 0 | 1 |
| 1999 | 1 | 1 | 2 |