Delta 3910

🇺🇸

Thor-Delta 3910

1:110 Scale

H:32.2 cmD:2.2 cm

~34 bricks tall~3 studs wide

Maiden Launch1980-02-14

Family: Delta

Designer: NASA·Manufacturer: McDonnell Douglas·Operator: NASA·Commissioner: NASA

2–3 Stages

Height / Length

35.4 m

Diameter

2.4 m

Launch Mass

195,000 kg

Takeoff Thrust

3,310 kN

LEO Capacity

2,700 kg

Mission Profile

The Delta 3910 (Thor-Delta 3910) was a two-to-three-stage American launch vehicle in the Delta family, featuring nine Castor IV solid rocket augmentation motors for enhanced first-stage performance. Standing 35.4 m tall with a 2.4 m diameter and a liftoff mass of 195 tonnes, it generated 3,310 kN of liftoff thrust and could deliver 2,700 kg to low Earth orbit. First flying in February 1980, the Delta 3910 provided a flexible mid-range capability and served as the basis for several PAM-equipped variants used throughout the 1980s.

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