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MCDONNELL DOUGLAS

Thor Delta A

2FLIGHTS
100%SUCCESS
2STREAK
Oct 1962FIRST FLIGHT
NOREUSABLE
HEIGHT31 m
DIAMETER2.44 m
LAUNCH MASS50 kg
LIFTOFF THRUST667 kN
STAGES3

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

250 kg
TO LEO
551 lbs
68 kg
TO GTO
150 lbs
667
KILONEWTONS
149,948
POUNDS-FORCE
~894
HORSEPOWER
Height31 m (102 ft)
Diameter2.44 m (8 ft)
Launch Mass50 kg (110 lbs)
Stages3