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Retired

Atlas V 421

Atlas V 421

🏭 United Launch Alliance🌐 American🔗 More Info📖 Wikipedia
Atlas V 421

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 421 version uses a 4m wide fairing, 2 solid rocket boosters and one engine on the Centaur stage.

📊 Specifications

📏Height
58.3 m
⭕Diameter
3.8 m
⚖️Launch Mass
433 kg
🛰️LEO Capacity
14,067 kg
🌍GTO Capacity
6,890 kg
🗓️Maiden Flight
Oct 11, 2007
🚀Total Launches
9
✅Success Rate
100%
♻️Reusable
Expendable
🏭Manufacturer
United Launch Alliance
🌐Country
American
📋Status
Retired

📷 Photo Gallery

Atlas V 421 photo 1

🛰️ Launch History