McDonnell Douglas

Thor Delta J

Delta J

Retired

Overview

/01

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

Manufacturer

McDonnell Douglas

Variant

Delta J

Alias

N/A

Maiden Flight

July 4, 1968

Technical Specifications

/02

31 m

Length

2.44 m

Diameter

0 t

Launch Mass

1452 kN

Liftoff Thrust

260 kg

LEO Capacity

263 kg

GTO Capacity

Launch Record

/03

1

Total Launches

1

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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