Thor Delta C1
Thor familyMcDonnell DouglasRetired
American orbital launch vehicle family with Thor first stage and a delta second stage.
Specifications
- Thrust
- 756 kN
- Height
- 27.5 m
- Diameter
- 2.44 m
- Launch mass
- 52 t
- Stages
- 3
- LEO capacity
- 81 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
100%success rate3 of 3
0failuresincluding partial failures
3success streakcurrent
First flight May 25, 1966 · latest January 22, 1969
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Thor Delta C1 flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 1966 | 1 | 0 | 1 |
| 1967 | 1 | 0 | 1 |
| 1968 | 0 | 0 | 0 |
| 1969 | 1 | 0 | 1 |