← ALL VEHICLES

MCDONNELL DOUGLAS

Thor Delta E

6FLIGHTS

100%SUCCESS

6STREAK

Nov 1965FIRST FLIGHT

NOREUSABLE

HEIGHT31 m

DIAMETER2.44 m

LAUNCH MASS69 kg

LIFTOFF THRUST1,452 kN

STAGES3

ABOUT THOR DELTA E

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

PAYLOAD CAPACITY

540 kg

TO LEO

1,191 lbs

150 kg

TO GTO

331 lbs

LIFTOFF THRUST

1,452

KILONEWTONS

326,423

POUNDS-FORCE

~1,947

HORSEPOWER

DIMENSIONS

↕Height31 m (102 ft)

↔Diameter2.44 m (8 ft)

⚖Launch Mass69 kg (152 lbs)

▣Stages3

FLIGHT HISTORY

Thor Delta E | ESSA 5

Apr 20, 1967SUCCESS

Thor Delta E | ESSA 4

Jan 26, 1967SUCCESS

Thor Delta E | ESSA 3

Oct 2, 1966SUCCESS

Thor Delta E | ESSA 2

Feb 28, 1966SUCCESS

Thor Delta E | Pioneer 6

Dec 16, 1965SUCCESS

Thor Delta E | GEOS A

Nov 6, 1965SUCCESS

🚀 OTHER MCDONNELL DOUGLAS VEHICLES

Delta 03003 flights Delta 09002 flights Delta 16042 flights Delta 19001 flights Delta 19131 flights Delta 19142 flights