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MCDONNELL DOUGLAS

Thor Delta L

2FLIGHTS
50%SUCCESS
1FAILURES
1STREAK
Aug 1969FIRST FLIGHT
NOREUSABLE
HEIGHT35 m
DIAMETER2.44 m
LAUNCH MASS89 kg
LIFTOFF THRUST1,452 kN
STAGES4

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

300 kg
TO LEO
662 lbs
300 kg
TO GTO
662 lbs
1,452
KILONEWTONS
326,423
POUNDS-FORCE
~1,947
HORSEPOWER
Height35 m (115 ft)
Diameter2.44 m (8 ft)
Launch Mass89 kg (196 lbs)
Stages4