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Ariane 5

Ariane 5

Space Launch Systems
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Basic Information
Name
Ariane 5
Designation
Ariane 5
Alternate Designation
A5 ECA, Ariane 5 ECA
Equipment Type
Space Launch Systems
Manufacturer
Arianespace
Date of Introduction
1996
Description

The Ariane 5 is the most advanced launch vehicle produced by the Arianespace consortium. It has been designed to meet current and future space access requirements for the commercial market. It can accommodate a dual 7,300 kg (16,093 lb) payload carrying it to Geosynchronous Transfer Orbit (GTO). The vehicle consists of a main cryogenic core stage that burns for over 600 seconds, two solid booster stages that provide 90% of thrust at the boost phase, and an upper stage. The versatile Ariane 5 launcher is able to deliver payloads to Low Earth Orbit (LEO), Medium Earth Orbit (MEO), GTO, and directly to Geosynchronous Orbit. France officials expects Ariane 5 to remain active until 2010 with about 64 launchers to be built and launched at a rate of 8-10 per year. The first Ariane 5 vehicle was launched in 1996 and failed. The second Ariane 5 was successfully launched in 1997 starting the commercial exploitation of this launch system. On May 10, 2004, EADS Space Transportation and Arianespace signed a contract for production and delivery of 30 Ariane 5 launchers worth €3 billion ($3.7 billion) at ILA 2004 in Berlin, Germany. The contract is a great significance commitment of European authorities with Ariane 5 launcher and space program. The launchers will be delivered between 2005 and 2010. In February 2005, ESA launched the first Ariane 5 ECA vehicle from the European spaceport in Kourou, French Guyana. The qualification flight V164 12-Feb-2005 put into orbit the Spanish satellite Xtar-EUR, the model Maqsat-2 and the micro satellite Sloshsat. Ariane 5 ECA or A5 ECA was the newest version of Ariane 5 launch system. The new version is equipped with the Vulcain 2 main engine and a new cryogenic upper stage, dubbed ESC-A. The development of Ariane 5 ECA began in December 2002 following V157 flight, which suffered a mishap resulting in the vehicle self-destruct, many improvements have been implemented on the new vehicle to make it safer and more reliable than the early version introduced in 2002.

Overview (Deagel)
Group Space Launch Systems
Status Retired - No Longer Operational
Also Known As A5 ECA, Ariane 5 ECA
Origin France
Contractor Arianespace
Initial Operational Capability (IOC) 1996
Total Production 117
Unitary Cost EUR €114 million
Specifications (Deagel)
Crew 0
Number of Stages 2
Dimensions — Height 54 meter
Dimensions — Rocket Diameter 4.8 meter
Mass — Max Lift-off Thrust 1,161 ton
Mass — Max Lift-off Weight 712 ton
Mass — Payload to GTO 8,000 kilogram
Variants
Variant 1 Ariane 1
Variant 2 Ariane 3
Variant 3 Ariane 2
Variant 4 Ariane 4
Variant 5 Ariane 5
Variant 6 Ariane 5 ME
Variant 7 Ariane 62
Variant 8 Ariane 64
Details
Country of Origin France
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
54 m
Width
4.8 m
Height
54 m
Weight
712000 kg
Operators (1)
France
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