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Thor Able II

Thor familyMcDonnell DouglasRetired

American orbital launch vehicle. Thor with Able stage derived from Vanguard second stage.

Thor Able II vehicle

Specifications

Thrust
668 kN
Height
27.3 m
Diameter
2.44 m
Launch mass
52 t
Stages
2

Specifications from Launch Library. Figures the operator has not published are omitted.

Flight record

2flightswith a definitive outcome
50%success rate1 of 2
1failureincluding partial failures
1success streakcurrent

First flight September 17, 1959 · latest April 1, 1960

Counted from padside's own launch record, the same basis as the stats page.

Flights per year

  • Successful
  • Failed
Show the numbers for Thor Able II flights per year
Thor Able II flights per year
YearSuccessfulFailedTotal
1959011
1960101

Flights

2 of 2