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Delta II

Satellite Launch Vehicle Platform by United Launch Alliance (4 more products)
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Delta II Image

The Delta II from United Launch Alliance is a Satellite Launch Vehicle Platform with Launch Vehicle Height 39 m/128 ft, Payload Capacity 1870 to 3470 Kg, Second Stage Engine Thrust 9753 lbs, Second Stage Engine ISP 320.5 Seconds. More details for Delta II can be seen below.

Product Specifications

Product Details

  • Part Number
    Delta II
  • Manufacturer
    United Launch Alliance
  • Description
    Delta II has launched many memorable missions including NASA’s rovers Spirit and Opportunity, the Phoenix Mars Lander, all operational GPS missions

General Parameters

  • Launch Vehicle Height
    39 m/128 ft
  • Payload Capacity
    1870 to 3470 Kg
  • Number of Stage
    Three Stage
  • First Stage Engine
    RS-27 A Engine
  • Second Stage Engine
    Aerojet AJ10-118K Engine
  • Second Stage Engine Thrust
    9753 lbs
  • Second Stage Engine ISP
    320.5 Seconds
  • Propellant
    Aerozine 50/N204
  • Space Heritage
    Yes

Technical Documents
View details on the manufacturer's website