McDonnell Douglas

Thor Delta C1

Delta C1

Retired

Overview

/01

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

Manufacturer

McDonnell Douglas

Variant

Delta C1

Alias

N/A

Maiden Flight

May 25, 1966

Technical Specifications

/02

27.5 m

Length

2.44 m

Diameter

0 t

Launch Mass

756 kN

Liftoff Thrust

81 kg

LEO Capacity

—

GTO Capacity

Launch Record

/03

3

Total Launches

3

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

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