National Aeronautics and Space Administration Logo
Follow this link to skip to the main content NASA Banner
Solar System Exploration
News & Events
Healthy Rosetta
Healthy Rosetta
4 Mar 2004
(Source: European Space Agency)

http://sci.esa.int/science-e/www/object/index.cfm?fobjectid=34797

Rosetta in Good Health
European Space Agency
March 4, 2004

Launch Summary

Ariane 5 Flight 158 lifted off right on-schedule at 07:17:51 UTC on 2 March carrying with it the Rosetta spacecraft on the start of its 10 year journey to comet Churyumov-Gerasimenko.

The solid boosters separated as expected at 07:20 UTC, followed 50 seconds later by the fairing. The first stage burn continued until 07:27 UTC and injected the EPS and Rosetta into a coast orbit. This was the first occasion that an Earth escape trajectory and a large delay until ignition of the upper stage has been flown by an Ariane 5 launch vehicle and the progress of the flight was monitored with mounting tension in the ESOC control centre.

The ignition of the EPS occurred 107 minutes after launch at 09:14 and was monitored from a ground station in Hawaii until the vehicle moved out of contact. Contact was made again from the Galliot station in Kourou and at 09:32:36 Arianespace announced the separation of Rosetta. The achieved orbit proved to be near perfect.

There was great joy and excitement in the ESOC control centre when the ESA Kourou ground station acquired the TM signal from Rosetta one minute later at 09:34. The spacecraft status was as expected and the automatic separation sequence was seen to be in progress. The venting and priming of the propulsion system was completed at 9:44.

Activation and Checkout

The initial spacecraft spin rate reduction and Sun acquisition phase proceeded very smoothly, and this was followed by the deployment of the two solar array panels, which was completed at 10:11. The separation sequence was completed with Sun reacquisition.

2 March 2004

10:34 Uplink of the first telecommands from the Kourou station Early Orbit Phase

11:25 Both star trackers switched on for first check

13:15 Both star trackers switched on to be used for attitude control

13:51 Spacecraft enters Safe Hold Mode

14:23 Reaction wheels switched on

14:47 Spacecraft commanded into Normal Mode

The launch locks of the Lander Philae have been released successfully at the end of the first ground station pass. Philae now remains firmly attached to the spacecraft by the cruise latches until its release at the comet.

3 March 2004

00:34 The High Gain Antenna was deployed, starting with firing the pyros of the launch locks. This was followed by 3 rotations, first in elevation, then in azimuth, and finally a combined azimuth and elevation movement, which brought the 2.2 m dish in the Earth pointing position.

09:34 The first trajectory correction manoeuvre was a test manoeuvre of 1 ms-1. The spacecraft was slewed to the required attitude in preparation for the 7 minutes burn.

11:49 Start of 7 minutes burn.

14:09 The attitude orbit control systems performed flawlessly throughout the manoeuvre and the spacecraft was back in its normal mode.

Due to the excellent spacecraft performance and the good progress of planned activities, it is anticipated to advance some of the planned form and payload commissioning.

This completed a very successful first phase of the mission. The spacecraft has behaved very much as expected. Both the Rosetta spacecraft and ground segment continued to perform excellently.

Orbit Trajectory

The spacecraft is travelling at a relative speed of 15 000 kmh-1 away from the Earth and it has passed a distance of 700 000 km. The specialists at ESOC have completed the initial orbit determination and confirmed the excellent injection to orbit by the Ariane 5 launch vehicle. The resulting orbital elements are as follows:

EPOCH (UTC) 2004/03/02 09:32:36 (separation from Ariane 5)

The Earth Equatorial J2000.0 State and Elements WRT Centre of the Earth

Position (km) X -3800.385690
Y -6686.243272
Z 764.805818
Velocity (kms-1) Xdot 6.740760
Ydot -8.376383
Zdot 0.312135

Semi Major Axis (km) -31756.626407
Eccentricity 1.213208
Inclination (?) 5.697642
Ascending Node (?) 145.741025
Argument of Pericentre (?) 55.326314
True Anomaly (?) 39.296396

Pericentre Distance (km) 6770.767019
Vinfinity (kms-1) 3.542841
Vinfinity Right Ascension (?) 346.486802
Vinfinity Declination (?) -2.024067

NOTE: All times are in UT

News Archive Search  Go!
Show  results per page
 
 
Awards and Recognition   Solar System Exploration Roadmap   Contact Us   Site Map   Print This Page
NASA Official: Kristen Erickson
Advisory: Dr. James Green, Director of Planetary Science
Outreach Manager: Alice Wessen
Curator/Editor: Phil Davis
Science Writer: Autumn Burdick
Producer: Greg Baerg
Webmaster: David Martin
> NASA Science Mission Directorate
> Budgets, Strategic Plans and Accountability Reports
> Equal Employment Opportunity Data
   Posted Pursuant to the No Fear Act
> Information-Dissemination Policies and Inventories
> Freedom of Information Act
> Privacy Policy & Important Notices
> Inspector General Hotline
> Office of the Inspector General
> NASA Communications Policy
> USA.gov
> ExpectMore.gov
> NASA Advisory Council
> Open Government at NASA
Last Updated: 5 Mar 2004