Delta II 7920-10C

Delta II 7920-10C is a expendable launch vehicle with its maiden flight in 1997. It has a payload capacity of 5,959 kg to low Earth orbit (LEO). It has completed 17 launches in its operational history.

Technical Specifications

  • Maiden flight: May 1997
  • Stages: 2
  • Height: 38.7 m
  • Diameter: 2.4 m
  • LEO capacity: 5,959 kg
  • GTO capacity: 1,842 kg
  • Type: Expendable

Launch History

17 total launches · 17 successful · 0 failed.

Upcoming Launches with Delta II 7920-10C

No launches currently scheduled.