Atlas V 500 Series

Launch Vehicle Platform by United Launch Alliance (4 more products)

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Atlas V 500 Series Image

The Atlas V 500 Series from United Launch Alliance is a Launch Vehicle Platform with Payload Capacity 2540 to 18850 Kg, First Stage Engine Thrust 860300 lbs, First Stage Engine ISP 311 Seconds, Second Stage Engine Thrust 22900 lbs, Second Stage Engine ISP 450.5 Seconds. More details for Atlas V 500 Series can be seen below.

Product Specifications

Product Details

  • Part Number
    Atlas V 500 Series
  • Manufacturer
    United Launch Alliance
  • Description
    Atlas V 500 Series uses a standard common core booster, a Centaur upper stage in a single or dual-engine configuration

General Parameters

  • Payload Capacity
    2540 to 18850 Kg
  • Number of Stage
    Two Stage
  • First Stage Engine
    RD 180 Engine
  • First Stage Engine Thrust
    860300 lbs
  • First Stage Engine ISP
    311 Seconds
  • Second Stage Engine
    RL10 Engine
  • Second Stage Engine Thrust
    22900 lbs
  • Second Stage Engine ISP
    450.5 Seconds
  • Propellant
    Liquid Oxygen, Liquid Kerosene, Liquid Hydrogen
  • Booster
    Aerojet Rocketdyne Solid Rocket Booster
  • Inclination
    0 Degrees (GEO), 27 Degrees (GTO), 28.7 Degrees (LEO), 90 Degrees (LEO), 51.6 Degrees (LEO ISS)
  • Space Heritage
    Yes

Technical Documents