Padside

Thor Delta D

Thor family · McDonnell Douglas · Retired

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

Specifications

Thrust
1,571 kN
Height
32 m
Diameter
2.44 m
Launch mass
63 t
Stages
4
Launch cost
$12.72M
LEO capacity
450 kg
GTO capacity
104 kg
GEO capacity
SSO capacity

Vehicle specifications from Launch Library; blanks are unpublished figures.

Flight record

Flights
2
Launches with a definitive outcome
Success rate
100%
2 of 2
Current success streak
2
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