Ariane 5 Launcher

Ariane 5 is a launcher developed and built under European Space Agency (ESA) licence by EADS SPACE Transportation.
The primary use of Ariane 5 is the geostationary orbit positioning of satellites. Two satellites can be loaded using the Sylda loader. Three satellites can also be loaded if they are small enough in weight and size. Up to eight secondary payloads can be carried, mainly small payloads with experiments or microsatellites that are loaded using the ASAP (Ariane Structure for Auxiliary Payloads) loader.
The main stage (EPC, Etage Principal Cryotermique) is, in its main components, a double tank and an engine. It is 30.5 metres high, 5.4 metres in diameter and has a fully loaded mass of approximately 170 tonnes. The propellant is stored in an upper tank (130 tonnes of liquid oxygen, at a temperature of -184 degrees centigrade) and a lower tank (approximately 25 tonnes of liquid hydrogen kept at -251 degrees centigrade). Through certain mechanisms, the two liquids are pumped into the combustion chamber, the heart of the Vulcain engine, which expels the gas produced by combustion at very high speed through a nozzle.
The Vulcain is considered one of Europe’s great technological successes. It alone cost a quarter of all the investment in the launcher programme, while 40 different European industries contributed to its construction. After ten minutes of uninterrupted thrust, the Vulcain shuts down, the first stage separates from the second stage and returns to Earth following a ballistic trajectory. Most of the first stage burns up in the atmosphere through friction, while what remains falls more than 2,000 km off the coast, in the middle of the Pacific Ocean.
The Vulcain is considered one of Europe’s great technological successes. It alone cost a quarter of all the investment in the launcher programme, while 40 different European industries contributed to its construction. After ten minutes of uninterrupted thrust, the Vulcain shuts down, the first stage separates from the second stage and returns to Earth following a ballistic trajectory. Most of the first stage burns up in the atmosphere through friction, while what remains falls more than 2,000 km off the coast, in the middle of the Pacific Ocean. During the first few minutes of the launch, the cryogenic engine provides just 8% of the necessary thrust. Most of the work is done by two lateral rocket boosters, the so-called boosters (EAP, Etage d’Accelerationà Poudre), which, at 30 metres high and 3 metres in diameter, devour 240 tonnes of propellant each in just over two minutes. After about 130 seconds from launch, at an altitude of about 55 kilometres, the two boosters are released from the main stage in controlled explosions and plunge into the Atlantic Ocean about 450 kilometres off Kourou. The boosters are also responsible for the changes in the launcher’s direction of travel, because the nozzle at the base of the engine is movable, being able to tilt about 6.5 degrees around the vertical. Unlike the main stage, the rocket boosters are fuelled by solid propellant, a compound consisting of ammonia perchlorate (68%), which acts as an oxidant, aluminium powder (18%), which acts as a reductant, and, finally, polybutadiene (14%), which acts as a binder and catalyst.

Ariane 5

Componente 1

Componente 2

Componente 2

Componente 3

Componente 4

Involucro in custom 450

Semicollare in bell 28" 150-600

Tappi e semicollare

Adapter

Adapter 2

Adapter 4

Adapter 5

Bolt Tension

Bolt Tension 2

Bolt Tension 2

Bolt Tension 3

Bolt Tension 3

Bush Floating

Bush Floating 2

Cover Drain

Cover Drain 2

Nut

Nut 2

Cover Helio

Cover Helio 2

Cover Helio 4

Distanziali

Distanziali 3

Distanziali 4

Distanziali 6

Rake-electrical

Seal

Seal 2

Turbopompa

Motore Vinci

Motore Vinci

Motore Vinci

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