A dataset provided by the European Space Agency

Name RO-X-SREM-5-PRL-COM
Mission INTERNATIONAL-ROSETTA-MISSION
URL ftp://psa.esac.esa.int/pub/mirror/pub/mirror/INTERNATIONAL-ROSETTA-MISSION/SREM/RO-X-SREM-5-PRL-COM-V1.0
DOI https://doi.org/10.57780/esa-fzvdhlx
Abstract This data set contains derived electron and proton flux energies in MeV from the Standard Radiation Environment Monitor (SREM) instrument on the Rosetta spacecraft. These are CODMAC Level 5 derived data, and measure the radiation in the spacecraft environment during the PRELANDING COMISSIONING mission phase.
Description Data Set Overview = This data set contains SREM omni-directional fluxes in MeV provided at particular effective energies, converted from the equivalent SREM Level 2 CDF products, which are provided in the EXTRAS directory. Note that the CDF processing levels differ from the CODMAC definition used within these PDS data sets. The SREM CDF Level 0 data are equivalent to the PDS CODMAC Level 2 data while the SREM CDF Level 2 data are equivalent to the PDS CODMAC Level 5 data. These data are useful for determining the energetic particle environment experienced by the Standard Radiation Environment Monitor onboard the Rosetta Orbiter. Processing Differential fluxes have first been derived from the 'raw' Level 0 CDF count rate data using a dedicated unfolding technique over pre-defined energies. The unfolding technique is based on the regularized Singular Value Decomposition (SVD) method described in [SANDBERGETAL2012], and in the SREMDC_FINAL_REPORT_V1.0.PDF file found in the DOCUMENT directory. The fluxes have then been rescaled according to cross-calibration studies between fluxes before a rescaling step against selected reference datasets. SEPEM Reference Dataset v2.0 (i.e. GOES/EPS fluxes cross- calibrated with IMP-8/GME) has been selected as reference for proton fluxes, while RBSP/MAGEIS spin averaged datasets were selected as a reference for electron fluxes. As a result of this process, the highest energy flux levels derived for the electron data were not reliable. Thus, it was decided to reject entirely these products in the production of this Level 5 data set. As such, only 10 energy channels are made available for electron fluxes. These are #1-#10 in the table on page 48 of the SREMDC_FINAL_REPORT_V1.0.PDF file, available in the DOCUMENT directory. A quality value is also provided alongside the fluxes, giving recommendations on their use, as described in the table below. FPDO: Flux Proto...
Instrument SREM
Temporal Coverage 2014-02-04T21:18:57Z/2014-05-06T23:57:40Z
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 Manoeuver 1 - Cruise phase 6 - Rendez-Vous Manoeuver 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 ...
Creator Contact M. BARTHELEMY, F. VALLEJO, D. HEATHER
Date Published 2020-12-01
Publisher And Registrant European Space Agency
Credit Guidelines European Space Agency, 2020-12-01, RO-X-SREM-5-PRL-COM, V1.0. https://doi.org/10.57780/esa-fzvdhlx