McDonnell Douglas

Thor Delta E

Delta E

Thor Delta E

Retired

Overview

/01

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

Manufacturer

McDonnell Douglas

Variant

Delta E

Alias

N/A

Maiden Flight

November 6, 1965

Technical Specifications

/02

31 m

Length

2.44 m

Diameter

0 t

Launch Mass

1452 kN

Liftoff Thrust

540 kg

LEO Capacity

150 kg

GTO Capacity

Launch Record

/03

6

Total Launches

6

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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