Ariane flight VA245


Ariane Flight VA245 is the Ariane 5 space launch of BepiColombo that took place on at 01:45:28UTC from the Guiana Space Centre. It was the launch of Ariane 5, and the Arianespace mission.

Payload

The payload of the launcher was the BepiColombo spacecraft. The total payload mass was approximately, including the payload adapter.

BepiColombo

BepiColombo had a liftoff mass of approximately. It comprises 3 different elements that will remain attached together during launch and cruise to Mercury: the Mercury Transfer Module, the Mercury Planetary Orbiter, and the Mercury Magnetospheric Orbiter. The assembly was accommodated inside the long version of the upper stage fairing. BepiColombo, a joint mission between ESA and JAXA, is Europe's first space mission to Mercury. The European modules were designed and manufactured by Airbus at its Friedrichshafen site in Germany as prime contractor for ESA, heading a consortium of 83 companies from 16 countries. The Japanese module was built by ISAS for JAXA. This flight was Airbus's mission, ESA's mission and spacecraft launched by Arianespace, and the latter's deep space mission.

Mission overview

Launch date

The Arianespace launch of took place on at 01:45:28UTC from Ariane Launch Complex No. 3 in Kourou, French Guiana.

Pre-flight activities

The different parts of the spacecraft arrived in French Guiana between April 24 and May 9. Deployment testing of BepiColombo MTM 2 solar arrays were performed at the Guiana Space Centre in the SC5 facilities. The MMO was integrated on the MPO between August 20 and 21. They were both integrated on the MTM between September 19 and 20 to complete BepiColombo. BepiColombo was assembled with its payload adapter on October 4, integrated on the launch vehicle on October 9, and enclosed within the fairing on October 11. The launch readiness review toko place on in Kourou to authorise the start of the final operations.

Orbit

The launch lasted 26 minutes and 47 seconds until separation, placing BepiColombo into a Mercury transfer orbit, escaping the Earth with a hyperbolic escape velocity of about and at an inclination of about -3.8 degrees. It is expected to be captured by and start orbiting Mercury approximately on, after a 7-year travel that will include several flybys of the Earth, Venus, and Mercury itself.