[meteorite-list] Rosetta in Good Health

From: Ron Baalke <baalke_at_meteoritecentral.com>
Date: Thu Apr 22 10:32:46 2004
Message-ID: <200403050023.QAA24202_at_zagami.jpl.nasa.gov>

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
            
Received on Thu 04 Mar 2004 07:23:44 PM PST


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