American orbital launch vehicle family with Thor first stage and a delta second stage.
Specifications
- Thrust
- 2,140 kN
- Height
- 34 m
- Diameter
- 2.44 m
- Launch mass
- 103 t
- Stages
- 3
- Launch cost
- $22.3M
- LEO capacity
- 355 kg
- GTO capacity
- 355 kg
- GEO capacity
- —
- SSO capacity
- —
Vehicle specifications from Launch Library; blanks are unpublished figures.
Flight record
Flights
12
Launches with a definitive outcome
Success rate
83.3%
10 of 12
Current success streak
7
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
- Thor Delta M | NATO IIB — Success
- Thor Delta M | Skynet IB — Success
- Thor Delta M | INTELSAT III F-8 — Success
- Thor Delta M | INTELSAT III F-7 — Success
- Thor Delta M | NATO IIA — Success