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Atlas V

Atlas V

Space Launch Systems
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Basic Information
Name
Atlas V
Designation
Atlas V
Alternate Designation
Atlas V-551, EELV, Evolved Expendable Launch Vehicle
Equipment Type
Space Launch Systems
Manufacturer
Lockheed Martin, Pratt & Whitney Rocketdyne, RD AMROSS
Date of Introduction
2002
Description

The Atlas V launch vehicle takes Lockheed-Martin expertise gained with Atlas and Titan programs. It can lift greater payloads (19,114-lb/8670 kg to GTO) than its predecessors (Atlas II and Atlas III). It uses the single-stage RD-180 engine and the new solid rocket booster known as the Common Core Booster. Lockheed-Martin designed the Atlas V to lift into orbit the heaviest satellites. The Atlas V consists of 400 and 500 series models. As of 2004, the US Air Force EELV program comprising the Delta IV and Atlas V launch vehicles was valued at $31.79 billion. As of early 2005, the Atlas V launch system had flown four successful commercial missions since its debut in August 2002. The fifth commercial launch was planned for March 2005 and the first US government launch was scheduled for April 2006. International Launch Services (ILS) had 16 EELV assignments. In early February 2005, ILS, a Lockheed-Martin joint venture, received green light from the US Air Force to launch a national security payload (NROL-24) on an Atlas V vehicle in mid-2007 from Cape Canaveral, Florida. This was one of seven launch services assigned to ILS and Atlas V vehicle under EELV program. As of March 2005, Atlas V had executed five flight missions. The fifth launch was carrying the Inmarsat 4-F1 6-ton satellite on March 11, 2005, through an Atlas V configured 431 meaning 4-meter-diameter fairing, three solid rocket boosters and a single-engine Centaur upper stage. In early June 2005, Aerojet and Lockheed-Martin were testing the Aerojet Solid Rocket Booster (SRB) Block B developed to provide enhanced performance and reliability to the Atlas V launch system. The Aerojet Block A SRBs were qualified in 2003 and had flown three successful missions. In January 2006, an Atlas V space launch system successfully propelled out of the atmosphere NASA's New Horizons spacecraft. This was the seventh flight assigned to Atlas V and the model involved was the Atlas V-551 which is powered by the Russian-built RD-180 main engine plus five solid rocket boosters. This Atlas commercial launch vehicle was provided by International Launch Services (ILS). Atlas V-551 model features more than 2 million pounds of thrust at the first stage. The ninth Atlas V rocket was launched from Cape Canaveral Air Force Station, Florida, on March 8, 2007. The space launch vehicle launched into orbit six satellites including: NextSat and ASTRO for DARPA; Space Test Program's STPSat-1; Los Alamos National Laboratory's CFESat; US Naval Academy's MidSTAR; and US Air Force Academy's FalconSat-3. The United States plans call for another 17 launches between 2024 and 2030 totaling 116 launches.

Overview (Deagel)
Group Space Launch Systems
Status Active
Also Known As Atlas V-551, EELV, Evolved Expendable Launch Vehicle
Origin United States of America
Contractors Lockheed Martin*, Pratt & Whitney Rocketdyne, RD AMROSS
Initial Operational Capability (IOC) 2002
Total Production 116
Unitary Cost USD $160 million
Specifications (Deagel)
Crew 0
Dimensions — Height 62.2 meter
Dimensions — Rocket Diameter 3.8 meter
Mass — Max Lift-off Thrust 860,200 pound
Mass — Max Lift-off Weight 562 ton
Mass — Payload to GTO 8,670 kilogram
Mass — Payload to LEO 18,850 kilogram
Gear (Deagel)
Item 1 Rocket Engines: GEM 63 (5)
Item 2 Rocket Engines: RD-180 (1)
Item 3 Rocket Engines: RL10A-4-2 (1)
Item 4 Spaceships: X-37B (1)
Variants
Variant 1 Atlas II
Variant 2 Atlas III
Variant 3 Atlas V
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
62.2 m
Width
3.8 m
Height
62.2 m
Weight
562000 kg
Operators (1)
United States
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