McDonnell Douglas

Thor Delta E1

Delta E1

Thor Delta E1

Retired

Overview

/01

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

Manufacturer

McDonnell Douglas

Variant

Delta E1

Alias

N/A

Maiden Flight

July 1, 1966

Technical Specifications

/02

28 m

Length

2.44 m

Diameter

0 t

Launch Mass

1450 kN

Liftoff Thrust

540 kg

LEO Capacity

150 kg

GTO Capacity

Launch Record

/03

17

Total Launches

16

Successful

1

Failed

94.1%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

← Back to Launchers