Warning: The magic method NinjaFormsAddonManager\WordPress\Plugin::__wakeup() must have public visibility in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-content/plugins/ninja-forms-addon-manager/lib/wordpress/plugin.php on line 22

Deprecated: Creation of dynamic property NinjaFormsAddonManager\Plugin::$service is deprecated in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-content/plugins/ninja-forms-addon-manager/includes/plugin.php on line 19

Notice: Function _load_textdomain_just_in_time was called incorrectly. Translation loading for the ninja-forms-uploads domain was triggered too early. This is usually an indicator for some code in the plugin or theme running too early. Translations should be loaded at the init action or later. Please see Debugging in WordPress for more information. (This message was added in version 6.7.0.) in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-includes/functions.php on line 6121

Deprecated: Implicit conversion from float 11.5 to int loses precision in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-includes/class-wp-hook.php on line 85

Deprecated: Implicit conversion from float 11.5 to int loses precision in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-includes/class-wp-hook.php on line 87

Notice: Function _load_textdomain_just_in_time was called incorrectly. Translation loading for the acf domain was triggered too early. This is usually an indicator for some code in the plugin or theme running too early. Translations should be loaded at the init action or later. Please see Debugging in WordPress for more information. (This message was added in version 6.7.0.) in /var/www/vhosts/sener.losdelvolcan.com/httpdocs/wp-includes/functions.php on line 6121
LISA Pathfinder. Data Management Unit - Sener
Ethics Hotline Contact

LISA Pathfinder. Data Management Unit

1 3
LISA Pathfinder. Data Management Unit
Client: European Space Agency (ESA)
Start date: 2024, December
Country: Spain

The Laser Interferometer Space Antenna (LISA) is a joint ESA/NASA mission to detect and observe gravitational waves in space and thus verify Einstein”s General Theory of Relativity.

The LISA core technologies are gravitational reference sensors, reactors that deliver micro-Newton thrust and laser interferometry. These technologies will be tested in space on the LISA Pathfinder Mission, which will comprise two instruments: the LISA Test Package (LTP) and the Disturbance Reduction System (DRS). Both of them will test the key “free-fall control”

Read more

The Laser Interferometer Space Antenna (LISA) is a joint ESA/NASA mission to detect and observe gravitational waves in space and thus verify Einstein”s General Theory of Relativity.

The LISA core technologies are gravitational reference sensors, reactors that deliver micro-Newton thrust and laser interferometry. These technologies will be tested in space on the LISA Pathfinder Mission, which will comprise two instruments: the LISA Test Package (LTP) and the Disturbance Reduction System (DRS). Both of them will test the key “free-fall control” technology by means of test masses.

Sener performed the design, integration and verification of the LTP”s Data & Diagnostics Subsystem, which includes:

  • The Data Management Unit (DMU) equipment with integrated software, tasked with:
  • Controlling the interferometer”s stability.
  • Acquiring the scientific data for monitoring.
  • Diagnostic equipment:
  • Diagnostic sensors for monitoring the LTP”s payload.
  • Sensor and actuation control.

The DMU performs:

  • The interface with the satellite”s on-board computer.
  • The Data Processing Unit (DPU), the on-board computer that controls the LTP”s operations.
  • Power Distribution Unit (PDU), responsible for the generation and distribution of voltages.
  • Data Acquisition Unit, DAU, which acquires the LTP”s environmental parameters (temperature, magnetic fields, and radiation).

Characteristics:

  • On-board computer based on a TSC695F CPU processor with 64 K x 8 bit PROM memories, 256 K x 32 bit EEPROM and 512 K x 40 bit SRAM, plus two MIL-STD-1553 interfaces and three asynchronous SBDL ports.
  • Data acquisition system to take measurements on 12 temperature channels with noise better than 10 μºK/√Hz and 16 analogue channels with a noise better than 230 μV/√Hz at 1 mHz.
Read less

Contact us

Contact us to find out how we can help you.