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MicroWave Radiometric Sounder (MiWaRS)
ESMO payload - URM_B2
Univ. La Sapienza / L'Aquila Team - Italy
ESMO project
In March 2006, the Education Department of the European Space Agency
approved the European Student Moon Orbiter (ESMO) mission proposed by the
Student Space Exploration & Technology Initiative (SSETI,
http://www.sseti.net/) association
for a Phase A Feasibility Study. If found to be feasible, ESMO will be the
third mission to be designed, built and operated by European students
through the SSETI association, and would join many other contemporary
missions to the Moon such as ESA’s SMART-1, the Chinese Chang’e-1, the
Indian Chandrayaan, JAXA’s SELENE and Lunar-A, and NASA’s Lunar
Reconnaissance Orbiter.
The ESMO mission objectives are summarised as follows: Education:
prepare students for careers in future projects of the European space
exploration and space science programmes by providing valuable hands-on
experience on a relevant & demanding project; Outreach: acquire
images of the Moon and transmit them back to Earth for public relations and
education outreach purposes; Science: perform new scientific
measurements relevant to lunar science & the future human exploration of the
Moon, in complement with past, present and future lunar missions;
Engineering: provide flight demonstration of innovative space
technologies developed under university research activities.
ESMO Sapienza web site
The general web site of ESMO Sapienza, including all teams, is: http://esmo.scepsi.it
MiWaRS payload
The MiWaRS payload, selected as a backup payload by SSETI at this stage, is thought to be a relatively light and simple instrument exploiting the feature of being substantially a low-noise receiver. In order to be allocated into ESMO Micro-Satellite and to fulfill the prescribed requirements, the MiWaRS may exhibit the following features:
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use of the nadir-pointing face of the a three-axis-stabilized Micro-Satellite in order to observe at the Moon surface; |
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use of antenna planar technologies, such as microstrip patch array, to realize an antenna gain between 6 and 18 dBi in order to compact instrument volume, still obtaining enough spatial resolution; horn and backfire antennas will be also considered; |
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use of multi-band antenna, tuned at different frequencies from C band up to K band (e.g., C, X, Ka and K channels), to realize a surface sounding capability; |
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use of a sufficiently long integration time in order to ensure a good radiometric accuracy of the order of few kelvins; |
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use of on-board radiometer calibration device or, in alternative, known stable microwave targets such as cosmic noise or specific features on the Moon surface, in order to perform the on-board instrument calibration; |
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use of COTS (Components Off The Shelf) and low-power components, in order to reduce overall costs and power consumption ; |
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use of an on-board data processing (filtering and compression) in order to adapt the data rate to downlink channel capacity |
The MiWaRS configuration may exploit either a usual total-power topology (with the advantage of simple realization, but a poor calibration), or a pulsed-noise injection topology (with the advantage of good self-calibration, but a more complex technological design).
MiWaRS Team
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Original proposal of La Sapienza to ESMO call |
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MiWaRS proposal to ESMO |
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Work Breakdown Structure (WBS) of current MiWaRS activities |
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MiWaRS Official Team:
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La Sapienza Team coordinators:
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MiWaRS Tutors
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MiWaRS objectives
Useful overview guides on Microwave Radiometry are:
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Some Internet hints on:
URM How To
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URM_B2 Mailing List (updated on 21-Mar-07) |
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How to connect to ESMO-NEWSGROUP: Instructions for MIRC |
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How to make a flow-chart within ECSS: Program |
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How to connect to the ESMO FTP site: ftp.sseti.net, https://portal.sseti.net/egroupware/login.php |
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LAST Update on the Web site: 21-Mar-07. |
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La Sapienza/L'Aquila team workshops |
Location and time |
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URM team recurrent meetings |
Every Wednesday - h. 15:00 Lab. of Ant., Remote Sens. & RadioProp. Dip. di Ing. Elettronica - 3° piano Fac. di Ingegneria "La Sapienza" - Rome |
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1st Plenary La Sapienza Team workshop (Giornate di studio) |
October 18-19, 2006 - h. 9:00 Saletta del Chiostro Fac. di Ingegneria "La Sapienza" - Rome |
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Meeting of URM Rome/L'Aquila team |
Wednesday - December 13, 2006 - h. 15:00 Aula 6 Fac. di Ingegneria "La Sapienza" - Rome |
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Meeting for 2nd ESMO workshop |
Wednesday - January 10, 2007 - h. 15:00 Aula 17 Fac. di Ingegneria "La Sapienza" - Rome |
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2nd Plenary La Sapienza Team workshop (II conference) |
March 20, 2007 - h. 9:00-18:00 Aula 1 "A. Ruberti" Fac. di Ingegneria "La Sapienza" - Rome |
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ESMO Team |
ESMO Standard Reports |
ESA Templates |
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URM team |
| Work Package | Title | Contents |
Personnel |
Deadline | Data |
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LUNAR MODELS WP1000 |
Physical models of lunar surface and sub-surface stratigraphy |
- Surface roughness and stratigraphy of lunar maria and terrae - Composition of lunar sub-surface (regolith, rocks, kreep ...) |
- F. De Gregorio - S. Carosi - B. Barresi Tutors: F. Marzano, N. PIerdicca |
December 31, 2006 | |
| Thermal models of lunar surface and sub-surface heat transport |
- Endo-thermal heat flux within lunar sub-surface - Eso-thermal heat flux on lunar surface |
- L. D'Amata - M. Cicchinelli Tutors: P. Tognolatti, F. Marzano |
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MICROWAVE MODELS WP1000 |
Microwave dielectric models of lunar surface and sub-surface material |
- Complex dielectric constant of lunar materials (regolith, rocks, kreep ...) - Distribution of lunar sub-surface material inhomogeneity |
- B. Barresi - S. Carosi Tutors: F. Marzano, N. Pierdicca |
January 31, 2007 | |
| Microwave emissivity and antenna temperature models of lunar surface and sub-surface |
- Incoherent models of lunar antenna noise temperature with 3 homogeneous layers - Incoherent models of lunar antenna noise temperature with multiple layers and scattering |
- S. Carosi - M. Montopoli - F. De Gregorio Tutors: F. Marzano, N. Pierdicca |
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RETRIEVAL ALGORITHMS WP1100 |
Physical retrieval algorithms of lunar surface and sub-surface parameters |
- Retrieval algorithms based on the inversion of physical-microwave models and their accuracy - Deconvolution algorithms for antenna overlapped field-of-view |
- S. Carosi - L. D'Amata - D. Canuzzi Tutors: N. Pierdicca, F. Marzano |
March 28, 2007 | |
| Statistical retrieval algorithms of lunar surface and sub-surface parameters |
- Retrieval algorithms based on the statistical inversion techniques - Expected accuracy of statistical algorithms based on synthetic data and MW-IR sensor integration |
- M. Montopoli - S. Carosi Tutors: F. Marzano, N. Pierdicca |
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RADIOMETER SYSTEM WP1100 |
Analysis and inter-comparison of radiometer system configurations |
- Selection of candidate radiometer configurations (total power, Dicke non-bal. and bal., noise-adding, integration with IR radiometer) - Matlab simulator to evaluate radiometric accuracy, sensitivity and criticality (calibration, thermal stability) |
- D. Canuzzi - G. De Donato - D. Sciumè - L. Di Marco Napini Tutors: N. Pierdicca, F. Marzano, P. Tognolatti |
March 31, 2007 | |
| Design and optimization of multi-frequency radiometer antenna |
- Selection of candidate multi-band antenna systems (microstrip patch arrays , horns, short back-fires) - Numerical optimization of antenna perfomances |
- A. Di Carlofelice - F. Equizi - S. Masci Tutors: P. Tognolatti, F. Marzano |
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RADIOMETER HARDWARE WP1200 |
Design and optimization of radiometer components and receiver |
- Analysis of the performances of radiometer layout components plus possible IR radiometer - Analysis and technical choice of optimal components |
- L. Di Marco Napini - D. Canuzzi Tutors: G. Perrotta, P. Tognolatti, F. Marzano, S. PIsa |
May 31, 2007 | |
| Analysis of MiWaRS production costs, feasibility and satellite compatibility |
- Analysis and choice of optimal components from cost/benefit analysis - Compatibility of radiometer with other satellite interfaces (data storage, power, stability, interference) |
- L. Di Marco Napini - D. Canuzzi Tutors: G. Perrotta, P. Tognolatti, F. Marzano
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RADIOMETER FEASIBILITY WP 1200 |
Overall evaluation of MiWaRS radiometer performances on multiple solution basis |
- Selection of multiple radiometer configuration and retrieval algorithms - Identification of the MiWaRS baseline and upgraded versions |
- ALL Tutors: F. Marzano, G. Perrotta, N. PIerdicca, P. Tognolatti |
June 30, 2006 End of the project |
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| Revision of mission objectives and lunar radiometer requirements |
- Mission objectives after feasibility study accomplishment - Baseline radiometer requirements satisfaction after feasibility study accomplishment - Proposal and set up of Terra-Luna experiments via MiWaRS |
- ALL Tutors: G. Perrotta, F. Marzano, P. Tognolatti, N. Pierdicca |