MTG. Scan assembly electronics (SCAE)

MTG. Scan assembly electronics (SCAE)

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Sener Space / Science & Earth observation / Spain
MTG. Scan assembly electronics (SCAE)
Client: ESA
Country: Spain

The main function of the MTG (Meteosat Third Generation) scan assembly electronics (SCAE) is to provide a controlled, high precision scan and sweep movement of the mirror of the main telescope.

To achieve this, the electronics house the following functions:

  • Accurate control and input of the dual axis motors: N/S (North/South) and E/W (East/West)
  • Control and input of blocking/unblocking motors of the mechanism
  • Monitoring and fault management
  • Communications with the spacecraft
  • Conditioning and internal distribution of power
  • Data processing and management 
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The main function of the MTG (Meteosat Third Generation) scan assembly electronics (SCAE) is to provide a controlled, high precision scan and sweep movement of the mirror of the main telescope.

To achieve this, the electronics house the following functions:

  • Accurate control and input of the dual axis motors: N/S (North/South) and E/W (East/West)
  • Control and input of blocking/unblocking motors of the mechanism
  • Monitoring and fault management
  • Communications with the spacecraft
  • Conditioning and internal distribution of power
  • Data processing and management 

Most of these functions take place in SW developed by SENER on a LEON2 platform. 

The unit consists of a nominal and a redundant section, both identical. Each of these sections houses the modules:

  • Modules:
  • DC/DC converter
  • Backplane, to interconnect modules
  • Processing module
  • Acquisition and motor drive module 
  • Mass: 5 Kg
  • Size: Length: 247; height: 150; width: 175
  • Thermal power:
    • Operating range: -20ºC: +50ºC
    • With start at – 25ºC
  • Redundancy: Two fully redundant sections in a single box.
  • Input: Input bus: +28 V
    • Power consumption: 25-30 W (approximate values according to the operating mode)
  • Observability and controllability:
    • Each section has various 1553 MilBus and SpaceWire communication buses for control and monitoring and dispatch of data, respectively
    • The unit implements a reduced set of PUS services
  • Features of the processing module:
    • Processor: LEON2 AT913E
    • Link SpW up to 80 Mbit/s (with capacity of 200 Mbit/s)
    • PROM memory: 32 kB
    • EEPROM memory: 4Mbit
    • SRAM memory: 5 MB (including fault detection and correction (EDAC)
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High Gain Antenna Gimbal (HGAG) for the rover Curiosity of the Mars Science Laboratory (MSL)

High Gain Antenna Gimbal (HGAG) for the rover Curiosity of the Mars Science Laboratory (MSL)

1 2
Sener Space / Communications in Space / Spain
High Gain Antenna Gimbal (HGAG) for the rover Curiosity of the Mars Science Laboratory (MSL)
Client: EADS-CASA
Start date: 2006, January
Country: Spain
End date: 2009, January

Sener participated in the Mars Science Laboratory (MSL) and his contribution was the development of the pointing mechanism of the High Gain Antenna Gimbal (HGAG).

The HGAG is a two degrees of freedom, elevation over azimuth, mechanical assembly that is located on the Curiosity rover top deck for precise pointing of the HGA, which enables the bidirectional communication directly between the Rover in Mars and the Earth.

Each degree of freedom is driven independently with a motorized mechanism to achieve desired speeds and accuracies.

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Sener participated in the Mars Science Laboratory (MSL) and his contribution was the development of the pointing mechanism of the High Gain Antenna Gimbal (HGAG).

The HGAG is a two degrees of freedom, elevation over azimuth, mechanical assembly that is located on the Curiosity rover top deck for precise pointing of the HGA, which enables the bidirectional communication directly between the Rover in Mars and the Earth.

Each degree of freedom is driven independently with a motorized mechanism to achieve desired speeds and accuracies.

The mechanism also incorporates a Hold Down and Release Mechanism (HDRM) which was released once the rover touches down the Martian ground (in August 2012).

In the frame of a Technical Assistance Agreement between the Jet Propulsion Laboratory (JPL) and the CDTI, Sener was responsible for the HGAG, with EADS-CASA Espacio as the main contractor of the High Gain Antenna Gimbal System (HGAS).

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Valle Office (Cádiz, Spain)

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Valle Office in CádizA-3899 Highway, 11.500 Km.Postal mail 5211580 San José del Valle (Cádiz, Spain)

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Valle 1 and Valle 2 parabolic through plants

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Valle Office in CádizA-3899 Highway, 11.500 Km.Postal mail 5211580 San José del Valle (Cádiz, Spain)

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Valle Office in CádizA-3899 Highway, 11.500 Km.Postal mail 5211580 San José del Valle (Cádiz, Spain)

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Format: jpeg

Valle Office in CádizA-3899 Highway, 11.500 Km.Postal mail 5211580 San José del Valle (Cádiz, Spain)

SENER offices in Cerdanyola del Vallès, Barcelona (Spain)

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Valle Office in CádizA-3899 Highway, 11.500 Km.Postal mail 5211580 San José del Valle (Cádiz, Spain)

Parabolic trough plant Casablanca

Parabolic trough plant Casablanca

1 7
Sener Energy / Renewable and Low-Carbon Solutions Generation / Solar / Spain
Parabolic trough plant Casablanca
Client: COBRA Sistemas y Redes (ACS)
Start date: 2011, January
Country: Spain
End date: 2013, January

Power generation plant of 50 MW located in Talarrubias, Badajoz, Spain.

The technology of the plant is parabolic through collectors. The owner is COBRA Systems y Reds (ACS). Sener is the EPC risk sharing partner and responsible for the complete design.

  • Project Data:
  • Total mirror surface: 510.000 m2.
  • Number of SCA/loops: 624/156 (SENERtrough®).
  • Field surface area: 195 Ha.
  • Nominal solar field thermal output: 262 MWt.
  • Thermal Storage Capacity: 1.010 MWht (7h).
  • Turbine capacity: 50 MWe.
  • Contract type: EPC.

Power generation plant of 50 MW located in Talarrubias, Badajoz, Spain.

The technology of the plant is parabolic through collectors. The owner is COBRA Systems y Reds (ACS). Sener is the EPC risk sharing partner and responsible for the complete design.

  • Project Data:
  • Total mirror surface: 510.000 m2.
  • Number of SCA/loops: 624/156 (SENERtrough®).
  • Field surface area: 195 Ha.
  • Nominal solar field thermal output: 262 MWt.
  • Thermal Storage Capacity: 1.010 MWht (7h).
  • Turbine capacity: 50 MWe.
  • Contract type: EPC.
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