Delta II 7920H

Delta II 7920H is a expendable launch vehicle with its maiden flight in 2003. It has a payload capacity of 5,959 kg to low Earth orbit (LEO). It has completed 1 launches in its operational history.

Technical Specifications

  • Maiden flight: August 2003
  • Stages: 2
  • Height: 38.9 m
  • Diameter: 2.44 m
  • Launch mass: 232 t
  • LEO capacity: 5,959 kg
  • GTO capacity: 2,120 kg
  • Type: Expendable

Launch History

1 total launches · 1 successful · 0 failed.

Upcoming Launches with Delta II 7920H

No launches currently scheduled.