The Atlas H was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was used to launch five clusters of NOSS satellites for the US National Reconnaissance Office. Two flights also carried LiPS satellites, as secondary payloads for the United States Naval Research Laboratory.
Specifications
- Thrust
- 2,282 kN
- Height
- 27 m
- Diameter
- 3.05 m
- Launch mass
- 150 t
- Stages
- 1
- Launch cost
- —
- LEO capacity
- 3,630 kg
- GTO capacity
- 2,255 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
5
Launches with a definitive outcome
Success rate
100%
5 of 5
Current success streak
5
Landings
0
0 attempts · 0 droneship / 0 RTLS
Fastest turnaround
—
Between consecutive booster flights
Counted from padside's own launch record — the same basis as the Stats page.
Launches
- Atlas H | Parcae 9A,B,C & MSD 9 — Success
- Atlas H | Parcae 8A,B,C & MSD 8 — Success
- Atlas H | Parcae 7A,B,C & MSD 7 — Success
- Atlas H | Parcae 6A,B,C & MSD 6 — Success
- Atlas H | Parcae 5A,B,C & MSD 5 — Success