McDonnell Douglas

Thor Delta A

Delta A

Retired

Overview

/01

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

Manufacturer

McDonnell Douglas

Variant

Delta A

Alias

N/A

Maiden Flight

October 2, 1962

Technical Specifications

/02

31 m

Length

2.44 m

Diameter

0 t

Launch Mass

667 kN

Liftoff Thrust

250 kg

LEO Capacity

68 kg

GTO Capacity

Launch Record

/03

2

Total Launches

2

Successful

0

Failed

100.0%

Success Rate

0

Attempted Landings

0

Successful Landings

0

Failed Landings

0

Consecutive Successes

← Back to Launchers