Delta 3920 PAM D

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Thor-Delta 3920/PAM-D

1:110 Scale

H:32.2 cmD:2.2 cm

~34 bricks tall~3 studs wide

Maiden Launch1982-08-26

Family: Delta

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

3 Stages

Height / Length

35.4 m

Diameter

2.4 m

Launch Mass

204,000 kg

Takeoff Thrust

3,310 kN

GTO Capacity

1,310 kg

Mission Profile

Delta 3920 PAM-D is a variant of the Thor-derived Delta family featuring a larger 2.4-meter fairing, Thiokol Castor IV strap-on boosters, and a McDonnell Douglas Payload Assist Module upper stage. The three-stage vehicle first flew on 26 August 1982 and was optimized for delivering commercial communications satellites to geostationary transfer orbit. It represents the evolution of the Delta rocket toward greater commercial launch capability in the early 1980s.

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