Thor Delta L
Thor familyMcDonnell DouglasRetired
American orbital launch vehicle family with Thor first stage and a delta second stage.
Specifications
- Thrust
- 1,452 kN
- Height
- 35 m
- Diameter
- 2.44 m
- Launch mass
- 89 t
- Stages
- 4
- Launch cost
- $16.54M
- LEO capacity
- 300 kg
- GTO capacity
- 300 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
2flightswith a definitive outcome
50%success rate1 of 2
1success streakcurrent
Counted from padside's own launch record, the same basis as the stats page.