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Atlas V

Atlas V

🏭 United Launch Alliance🌐 American🔗 More Info
Atlas V

Atlas V is an expendable launch system in the Atlas rocket family. It was formerly operated by Lockheed Martin and is now operated by United Launch Alliance (ULA), a joint venture with Boeing. Each Atlas V rocket uses a Russian-built RD-180 engine burning kerosene and liquid oxygen to power its first stage and an American-built RL10 engine burning liquid hydrogen and liquid oxygen to power its Centaur upper stage. The RD-180 engines are provided by RD Amross, while Aerojet Rocketdyne provides both the RL10 engines and the strap-on boosters used in some configurations. The standard payload fairing sizes are 4 or 5 meters in diameter and of various lengths. Fairings sizes as large as 7.2 m in diameter and up to 32.3 m in length have been considered. The rocket is assembled in Decatur, Alabama and Harlingen, Texas.

📊 Specifications

📏Height
60 m
⭕Diameter
—
⚖️Launch Mass
650 kg
🛰️LEO Capacity
—
🌍GTO Capacity
—
🗓️Maiden Flight
—
🚀Total Launches
0
✅Success Rate
0%
♻️Reusable
Expendable
🏭Manufacturer
United Launch Alliance
🌐Country
American
📋Status
Active

📷 Photo Gallery

Atlas V photo 1

🛰️ Launch History