A dataset provided by the European Space Agency

Name RO-C-RSI-1_2_3-PRL-0347
Mission INTERNATIONAL-ROSETTA-MISSION
URL ftp://npsa01.esac.esa.int/pub/mirror/INTERNATIONAL-ROSETTA-MISSION/RSI/RO-C-RSI-1_2_3-PRL-0347-V1.0
DOI 10.5270/esa-dyuyp3v
Abstract This is a Rosetta Radio Science data set, collected during the PRELANDING phase 2014-01-21 to 2014-11-18. It is a Global Gravity measurement at the comet 67P and covers the time 2014-10-10T04:52:05.000 to 2014-10-10T15:25:36.000.
Description Data Set Overview The Rosetta (RO) Radio Science (RSI) Data Archive is a time-ordered collection of raw and partially processed data collected during the Rosetta Mission to Churymov-Gerasimenko. For more information on the investigations see the RSI User Manual [RSIUSERMANUAL2004] in the DOCUMENT/RSI_DOC folder. This is a Global Gravity measurement covering the time 2014-10-10T04:52:05.000 to 2014-10-10T15:25:36.000. This data set was collected during the Rosetta Mission Prelanding Phase (PRL) - on route to comet Churymov-Gerasimenko. For more information about RSI measurements see INST.CAT or the RSI User Manual [RSIUSERMANUAL2004]. Mission Phase Definition Mission phase abbreviations are defined in CATALOG/MISSION.CAT and DOCUMENT/ESA_DOC/RO_EST_TN_3372.PDF. General description of radio science data = Closed-loop and Open-loop data: There are in principle two different ways to record radio science data: Open-loop and closed-loop data. The CLOSED-LOOP system used a phase-lock loop in the receiver to track the downlink signal, reporting both amplitude and fre- quency at rates typically of 1-10 times per second. In the OPEN-LOOP system, the signal was simply converted to a baseband frequency range; the entire passband was sampled and recorded for later processing. Typical open-loop sampling rates for ROS were 2000 complex samples per second. CLOSED-LOOP data are efficient for characterizing slowly changing signals; OPEN-LOOP data (because of their much higher volume) are usually used when the signal is very dynamic - such as during an occultation or bistatic radar measurement. The data set includes four primary data types with respect to the two different ground station systems. These systems are on the one hand the ESA ground station in New Norcia, Australia (NNO) and the NASA Deep Space Network (DSN). C...
Instrument RSI
Temporal Coverage 2014-10-10T04:52:05Z/2014-10-10T15:25:36Z
Version V1.0
Mission Description TABLE OF CONTENTS ---------------------------------- = ROSETTA Mission Overview = ROSETTA Mission Objectives - Science Objectives = Mission Profile = Mission Phases Overview - Mission Phase Schedule - Solar Conjunctions/Oppositions - Payload Checkouts = Mission Phases Description - Launch phase (LEOP) - Commissioning phase - Cruise phase 1 - Earth swing-by 1 - Cruise phase 2 (and Deep Impact) - Mars swing-by - Cruise phase 3 - Earth swing-by 2 - Cruise phase 4 (splitted in 4-1 and 4-2) - Steins flyby - Earth swing-by 3 - Cruise phase 5 - Lutetia flyby - Rendez-Vous Manouver 1 - Cruise phase 6 - Rendez-Vous Manouver 2 - Near comet drift (NCD) phase - Approach phase - Lander delivery and relay phase - Escort phase - Near perihelion phase - Extended mission = Orbiter Experiments - ALICE - CONSERT - COSIMA - GIADA - MIDAS - MIRO - OSIRIS - ROSINA - RPC - RSI - VIRTIS - SREM = LANDER (PHILAE) - Science Objectives - Lander Experiments = Ground Segment - Rosetta Ground Segment - Rosetta Science Operations Center - Rosetta Mission Operations Center - Rosetta Lander Ground Segment - Lander Control Center - Science Operations and Navigation Center - Rosetta Scientific Data Archive = Acronyms ROSETTA Mission Overview = The ROSETTA mission is an interplanetary mission whose main objectives are the rendezvous and in-situ measurements of the comet 67P/Churyumov-Gerasimenko, scheduled for 2014/2015. The spacecraft carries a Rosetta Lander, named Philae, to the nucleus and deploys it onto its surface. A brief description of the mission and its objectives can be found in [GLASSMEIERETAL2007A]. A detailed description of the mission analysis can be found in the ROSETTA User Manual [RO-DSS-MA-1001], and the flight Operations Plan [RO-ESC-PL-5000]. On its long way to the comet nucleus after a Launch by Ariane 5 P1+ in March 2004, the ROSETTA spacecraft orbited the Sun fo...
Creator Contact MARTIN PAETZOLD
Date Published 2017-02-08T00:00:00Z
Publisher And Registrant European Space Agency
Credit Guidelines European Space Agency, 2017-02-08T00:00:00Z, RO-C-RSI-1_2_3-PRL-0347, V1.0. https://doi.org/10.5270/esa-dyuyp3v