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Ariane 5 flight V195
Enabling & Support

Ariane 5’s second launch of 2010

27/06/2010 390 views 0 likes
ESA / Enabling & Support / Space Transportation

Yesterday evening, an Ariane 5 launcher lifted off from Europe’s Spaceport in French Guiana on its mission to place the Arabsat-5A telecommunications satellite and the multi-mission COMS satellite into their planned transfer orbits.

Liftoff of V195, the 51st Ariane 5 flight, came at 23:41 CEST (21:41 GMT; 18:41 French Guiana). The target orbit had a perigee altitude of 250 km and an apogee altitude of 35 958 km, inclined at 2º to the equator. The satellites were accurately injected into their transfer orbits about 26 minutes and 32 minutes after liftoff, respectively.

Arabsat-5A will be positioned in geostationary orbit above the equator at 30.5°E to provide telecommunications and TV broadcasting services in the Middle East and North Africa in the Ku- and C bands. South Korea’s COMS, to be positioned in geostationary orbit over 128.3°E, carries three payloads dedicated to meteorology, ocean observation and telecommunications.

Satellites in a circular orbit with an altitude of 35 800 km keep pace with Earth’s rotation and appears stationary when observed from the Earth, hence 'geostationary'.

The payload mass for this launch was 8393 kg: the satellite’s totalled 7315 kg, with payload adapters and dispensers making up the additional 1078 kg.

Arianespace and Europe’s Spaceport are planning four more Ariane launches in 2010, maintaining the heavy-lift vehicle’s flight rate. The ability to sustain high launch rates has already been demonstrated: during the 12-month period from August 2007 to August 2008 there were nine launches (V177 – V185).

V195 flight timeline

Ariane 5’s cryogenic, liquid-propellant main engine ignited first. Seven seconds later, the solid-propellant boosters also fired, and the vehicle lifted off a fraction of a second later.

The solid-propellant boosters were jettisoned 2 min 20 sec after main engine ignition, and the fairing protecting the payload during the climb through Earth’s atmosphere was discarded at 3 min 9 sec. The launcher’s main engine shut down at 8 min 55 sec; six seconds later, the main cryogenic stage separated from the upper stage and its payload.

Four seconds after main stage separation, the engine of the cryogenic upper stage was ignited to continue the journey. This engine shut down 24 min 40 sec into the flight, at which point the vehicle was travelling at 9416 m/s (33 898 km/h) at an altitude of 581.8 km – and geostationary transfer orbit had been achieved.

At 26 min 39 sec, Arabsat-5A separated from the upper stage, followed by COMS at 32 min 38 sec. Ariane 5’s flight was formally completed 49 min 52 sec after main engine ignition.

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