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Thor Delta A

Thor familyMcDonnell DouglasRetired

American orbital launch vehicle family with Thor first stage and a delta second stage.

Thor Delta A vehicle

Specifications

Thrust
667 kN
Height
31 m
Diameter
2.44 m
Launch mass
50 t
Stages
3
Launch cost
$9.59M
LEO capacity
250 kg
GTO capacity
68 kg

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

Flight record

2flightswith a definitive outcome
100%success rate2 of 2
2success streakcurrent

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

Flights

2 of 2