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Atlas · Convair

Atlas V 551

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Specifications

Status
active
Height
59.7 m
Diameter
3.8 m
Mass
573,000 kg
Stages
2
Payload to LEO
18,850 kg
Payload to GTO
8,890 kg
First flight
2006-01-19
Total launches
22
Success / Fail
22 / 0

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.

Payloads it launched · 226

KUIPER-00596
LEO
KUIPER-00602
LEO
KUIPER-00282
LEO
KUIPER-00383
LEO
KUIPER-00606
LEO
KUIPER-00603
LEO
KUIPER-00593
LEO
KUIPER-00562
LEO
KUIPER-00581
LEO
KUIPER-00610
LEO
KUIPER-00618
LEO
KUIPER-00595
LEO
KUIPER-00597
LEO
KUIPER-00584
LEO
KUIPER-00527
LEO
KUIPER-00608
LEO
KUIPER-00599
LEO
KUIPER-00605
LEO
KUIPER-00607
LEO
KUIPER-00572
LEO
KUIPER-00600
LEO
KUIPER-00613
LEO
KUIPER-00594
LEO
KUIPER-00570
LEO