Institute of Microgravity Ignacio Da Riva
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General information

Universidad Politécnica de Madrid

Description

IDR/UPM is a Research Institute of Universidad Politécnica de Madrid whose R&D activities aerospace technology include:
Design, construction, qualification and operation of spacecraft.
Payload development.
Engineering support in subsystems such as thermal control, structures, attitude and orbit determination and control.
Testing of space systems and equipment: thermal vacuum, vibrations.

IDR/UPM leads the Master in Space Systems (MUSE), a PBL official master course of UPM.

Summary of Research Services

Design, construction, qualification and operation of spacecraft.
Payload development.
Engineering support in subsystems such as thermal control, structures, attitude and orbit determination and control.
Testing of space systems and equipment: thermal vacuum, vibrations.

Technology Capabilities

Mission analysis and design

Attitude and orbit determination and control

Thermal control

Space structues and mechanical systems

Main equipment or Facilities

Software, tools or licenses to be applied to Big Science
Simulation tools (PATRAN/NASTRAN, ESATAN, CATIA, ESACRACK, ESACOMP, VAONE, etc.).
Concurrent Design Facility OCDE (Open concurrent Design environment).

Integration clean room.

Space environment test facilities:
Shakers:
Electrodynamic shaker with a hydrostatic-bearing slip table. For horizontal and three-axis testing and a loading capability of 17 kN.
Electrodynamic shaker for vertical vibrations of up to 7 kN.
Thermal vacuum chamber: 1 m3 useful testing volume, up to 5x10-6 mbar and temperature range from – 150 ◦C to 150 ◦C.

Concurrent Design Facility: integrated tool to perform systems engineering and mission design analysis in the early mission stages in a reduced time frame.

Contracts for Big Science facilities

[ESA] University space mission for the microsatellite launch UPMSat-3 (2024 - 2024)
Design, development, integration, launch and operation of micro-satellites UPMSat-3. (UPMSat-2, UPMSat-1). IP: Ángel Pedro Sanz Ándres
[ESA - NASA] Development of the thermal control and structural subsystems of two different instruments of the Solar Orbiter mission, launched in January 2020 (Solar Orbiter mission). ()
[ESA - Roscosmos] Development of the thermal control and structural subsystems of the instrument NOMAD (ExoMars mission). ()
[ESA - OSIRIS] Development of the thermal control subsystem of the instrument OSIRIS (Rosetta mission). ()
[ESA] Development of the thermal control and structural subsystems of the instrument ARIEL (Ariel mission). ()

Relevant R&D projects

[AEI] Solar physics and space weather (ARIEL_Ci3Tec ) (2024)
PID2024-158486OB-C33 (IP: Javier Pérez Álvarez )
[UPM] UPMSat-2
Microsatellite (50 kg) fully developed at IDR/UPM to be launched in March 2020.
[UPM] UPMSat-1
Microsatellite (50kg) fully developed at IDR/UPM launched in 1995.
[ESA-NASA] Solar Orbiter mission
Instruments PHI and EPD: thermal control and structural design. To be launched in February 2020.
[ESA-Roscosmos] ExoMars 2016 mission
Instrument NOMAD: thermal control and structural design. Launched in 2016.
[ESA] Rosetta mission
Instrument OSIRIS: thermal control. Launched in 2004.
[ESA] ARIEL mission
Telescope Assembly: thermomechanical design. To be launched in 2028.
[GALILEO] Set-up a GALILEO Information Centre in Chile
[GALILEO] Performance of a market study of different countries in the region to evaluate the possibilities of utilization of Galileo in different sectors and with different applications

Big Science Areas