Delta 3910 PAM D

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Thor-Delta 3910/PAM-D

1:110 Scale

H:32.2 cmD:2.2 cm

~34 bricks tall~3 studs wide

Maiden Launch1980-11-15

Family: Delta

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

3 Stages

Height / Length

35.4 m

Diameter

2.4 m

Launch Mass

195,000 kg

Takeoff Thrust

3,310 kN

GTO Capacity

1,085 kg

Mission Profile

The Delta 3910 PAM D (Thor-Delta 3910/PAM-D) was a three-stage American launch vehicle in the Delta family, combining the Delta 3910 core with a Payload Assist Module-Delta upper stage for geostationary transfer capability. 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 1,085 kg to geostationary transfer orbit. First flying in November 1980, the Delta 3910 PAM D was widely used for deploying commercial communications satellites in the early Shuttle era.

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