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Facilities

Instalaciones DEEYS

Those indicated in each of the Department's areas/laboratories.

FACILITIES - Electromagnetic Compatibility Tests

Electromagnetic Compatibility Facilities

Name Main Features

Semi-anechoic chamber

(FÉNIX)

Dimensions: L7 m x W3.8 m x H2.4 m

Semi-anechoic chamber

(ATENEA)

Dimensions: L24 m x W14 m x H10 m

Access door: W3,600 x H3,000

ISO 8 class

Electromagnetic Aggressions Laboratory

Electromagnetic pulse (EMP) up to 50 kV/m

Electrostatic discharge testing up to 300 kV

Lightning Indirect effects on equipment

Reverberation chamber (MTC)

Dimensions: L7.5 m x W5.5 m x H4.5 m

Frequency range: 100 MHz and 40 GHz

Small reverberation chamber (SMTC)

Dimensions: L4.08 m x W1.84 m x H1.76 m

Frequency range: 400 MHz and 40 GHz

Open Area Test Site

(OATS) 

2,500 m² platform (50 m x 50 m)

Connected to the Torrejón Air Force Base runway

Integration room

Dimensions: L7.5 m x W12 m x H6.5 m

Access door: 6 m x 6 m

ISO 8 class

 

Campaña de ensayos de EMC. Lanzador Vega C (CRISA / AVIO)

EMC testing campaign Vega C launcher (CRISA/AVIO)

Campaña de ensayos de Autocompatibilidad. Lanzador Vega (CRISA / AVIO)

Autocompatibility testing campaign Vega launcher (CRISA/AVIO)

Ensayos de EMC sobre la torre del sistema Sentinel 30 (EM&E)

EMC testing on the Sentinel 30 system tower (EM&E)

FACILITIES - Environmental Testing

The main facilities listed below are available for each of the testing services detailed above:

Mechanical Environmental Testing

Vibration Testing Facilities

Name Main Features

DUAL vibration system

Maximum acceleration: 12 g/s

Sliding table dimensions: 3 m x 3 m

ISO class 8

COMBO vibration system

Maximum acceleration: 30 g/s

Sliding table dimensions: 1.5 m x 1.2 m

Expander dimensions 1.2 m Ø

COMBO 2 vibration system

“CANIS MAJOR”

Maximum acceleration: 40 g/s

Sliding table dimensions: 0.8 m x 0.8 m

Expander dimensions 0.8 m Ø

Vertical vibration system

Maximum acceleration: 26 g/s

Expander dimensions 1: 2.3 m x 2.3 m

Expander dimensions 2: 1.5 m x 1.5 m

 

Exomars Shield (AIRBUS DS)

Vibration testing on the DUAL system of the Exomars Shield (AIRBUS DS)

Cubesat Proyecto ANSER (INTA)

Vibration testing of Cubesat ANSER Project (INTA)


SRS Shock Facilities

Name Main Features

Pneumatic SRS system

“MESSIER 82”

Maximum acceleration: 100,000 g/s

Maximum specimen dimensions: 300 mm x 300 mm x 300 mm

Maximum weight EUT: 45 kg

 

Sistema neumático de choque (INTA)

Pneumatic shock system


Mechanical Environmental Testing (Physical properties)

Physical Properties Determination Facilities

Name Main Features

SPIDER 35 scale

Maximum specimen dimensions: 400 mm x 300 mm

Maximum weight EUT: 35 kg

SPIDER 600 scale

Maximum specimen dimensions: 1,250 mm x 1,000 mm

Maximum weight EUT: 600 kg

Centre of gravity measurement system

 SCHENCK ESE

Maximum specimen dimensions: Ø 1,000 mm

Maximum weight EUT: 60 kg

Centre of gravity measurement system

SCHENCK WS 4

Maximum specimen dimensions: Ø 1,000 mm

Maximum weight EUT: 400 kg

Moment of inertia measurement system

SCHENCK M2

Maximum specimen dimensions: Ø 500 mm

Maximum weight EUT: 40 kg

Moment of inertia measurement system

SCHENCK M4

Maximum specimen dimensions: Ø 1,000 mm

Maximum weight EUT: 400 kg


Climatic Environmental Testing

Thermal cycling facilities in vacuum/inert atmosphere

Name Main Features

CENTAURUS A simulator

Dimensions: 4 m x 4 m x 4 m

Temperature range: -170°C to +150°C

Vacuum level: <10-5 Pa

Thermoelastic testing capability

ANDROMEDA simulator

Dimensions diameter: 2 m x 3 m depth

Temperature range: -190°C to +150°C

Thermal plate: -150º to +150ºC

Vacuum level: <10-5 Pa

COSMOS 01 simulator

Dimensions diameter: 1.3 m x 1.5 m depth

Temperature range: -155°C to +150°C

Thermal plate: -150º to +150ºC

Vacuum level: <10-5 Pa

COSMOS 02 simulator

Dimensions diameter: 0.8 m x 1 m depth

Temperature range: -155°C to +150°C

Vacuum level: <10-5 Pa

BIG MAGALLANES

Dimensions: 1.45 m x 1.42 m x 1.5 m

Temperature range: -170°C to +170°C

Ambient pressure in a GN2 atmosphere

LITTLE MAGALLANES

Dimensions: 0.815 m x 0.815 m x 0.535 m

Temperature range: -170°C to +170°C

Ambient pressure in a GN2 atmosphere

DRACO ATC4

Dimensions: 0.280 m x 0.330 m x 0.140 m

Temperature range: -180°C to +150°C

Ambient pressure in a GN2 atmosphere

 

Ensayo de vacio térmico INTA

Thermal vacuum test on large deployable antenna LEA H2020  programme

Programa ANSER

Thermal vacuum test. ANSER programme

Ensayo de deformaciones termoelásticas de Feeder SubAssembly

Thermoelastic distortion testing of Feeder SubAssembly (AIRBUS DS)

satlélite DEIMOS 2

DEIMOS 2 satellite thermal vacuum test

Ciclado térmico en TVAC ANDROMEDA

Thermal cycling in TVAC ANDROMEDA – PLATO FM23 programme

Choque térmico en “DRACO-ATC4

Thermal shock in ‘DRACO-ATC4’ – SPASOLAB Solar Cells (20P024)

Ensayo de fotogrametría INTAEnsayo de fotogrametría

Photogrammetry test on satellite communication system (AIRBUS DS)

FACILITIES - Electrical Test, Space RF power and SPASOLAB

Ensayos Eléctricos

Electrical Tests Facilities

Name Main Features

Climate chamber

Dimensions: 5,600 x 3,000 x 3,000 mm

Range: Temperature: -60 to +110°C; Humidity: 10% to 95%

Maximum DUT weight: 400 kg/m²

Maximum temperature variation slope: 2°C/min

Three-phase power supply High-power testing

 

Output: DC, AC, DC+AC

Output power: 90 kVA AC, 60 kW DC

Output voltage: Up to 300 VFN

Output current: Up to 200A per phase

Output frequency: 16 Hz to 905 Hz

 

 

Ensayos climáticos

SIVA certification climate testing in a large climate chamber

Ensayos climáticos

MILANO certification climate tests in a large climate chamber


Space RF power

Space RF power Facilities

Name Main Features

Radiated PIM test chamber with temperature

External camera dimensions (PIM without temperature): 5 x 5 x 3.3 m

Dimensions of PIM interior chamber with temperature: 1,000 x 1,800 x 1,800 mm

Maximum weight DUT: 200 kg

Temperature-RH range: -150 to +150°C; 50% to 0% RH

Maximum average speed temperature variation: 2°C/min

 

MULCOPOWER thermal vacuum chamber for multipactor, corona and power handling tests

 

Dimensions: Diameter: 1 metre, height: 0.5 metres

Maximum DUT weight: 100 kg/m²

Temperature-Pressure range: -60 to 90°C; 1,000 to 10-6 mb

ISO C8 clean room

Temperature, humidity and pressure control

Dimensions: Approximately 100 m²

High-power amplifiers

100 MHz – 1 GHz: 2.5 kW continuous and pulsed

1 GHz – 18 GHz:      1 kW continuous, 7 kW pulsed

18 GHz – 40 GHz: 350 W continuous and pulsed

 

 

Cámara anecoica

Anechoic chamber for PIM testing at temperature

Cámara TVAC

TVAC chamber for multipactor testing in clean rooms

antena SARANT para GALILEO (SENER)

PIM test on the SARANT antenna for GALILEO (SENER)

Banco de ensayo PIM

PIM test bench


Space Photovoltaic Testing

 

Space Photovoltaic Testing Facilities

Name Main Features

Continuous light solar simulators

Spectral zone: Up to 4 zones

Sunspot: Up to 300 mm

Spectrum: AM0, AM1.5, variable spectrum

Pulsating light simulator

Xenon lamps

Coupon and panel measurement

Maximum size EUT: 2 x 2 m

Spectral response measurement system

Maximum size DUT: 150 x 150 x 20 mm

Spectral range: 280 – 1,900 nm

Temperature range: -180°C to +200°C (with cryostat)

Maximum equivalent current: 10 mA

UV degradation test chamber

Temperature range: -30°C to 300°C

Pressure: up to 10-6 mbar (high vacuum)

Solar radiation intensity: up to 13 SC

 

Thermo-optical property measurements

Spectrophotometer based on a double monochromator

Spectral range: 200 – 2,500 nm

Spectrum measurements

Continuous sources of light and solar radiation

Spectral range: 250 – 1,700 nm

 

ensayos a células solares

High/low temperature chamber variable between -160ºC and +300ºC for solar cell testing

Cámara de alta/baja

Cryostat for high/low temperature spectral response measurements

Radiación Ultravioleta

Ultraviolet radiation chamber

Simulador Solar Triple Fuente

Triple-source solar simulator with low irradiance set-up

FACILITIES - RadioFrequency Tests

Radiofrequency Tests Facilities

Name Main Features

Compact anechoic chamber

 

Dimensions: L30.5 m x W18 m x H13 m

Quiet zone: L6 m x W5.5 m x H5 m

Antenna measurement, frequency range: 1.5 GHz to 40 GHz

Radar signature, frequency range: 1.5 GHz to 40 GHz

SNF, maximum antenna size: 8 m, frequencies: 0.4 GHz to 40 GHz

Near spherical field

Dimensions: L7 m x W4 m x H4 m

Antenna measurement, frequency range: 0.4 GHz to 40 GHz

Semi-open anechoic chamber

Dimensions: L12 m x W12 m x H12 m

Frequency range: 1 GHz to 40 GHz

Open field antenna measurement range

Frequency range: 80 MHz to 3 GHz

BIANCHA anechoic chamber

Dimensions: L7.1 m x W6.3 m x H3.9 m

Frequency range: 800 MHz to 26.5 GHz

Complete bi-static hemispheric system

POLYBENCH

Maximum sample dimensions: 500 mm x 500 mm

Frequency range: 2.6 GHz to 40 GHz

High-precision installation (< 0.05 dB)

POLYBENCH mmW

Maximum sample dimensions: 500 mm x 500 mm

Frequency range: 50 GHz to 110 GHz

High-precision installation (< 0.1 dB)

MsJOINTS

Maximum sample dimensions: 396 mm x 260 mm

Measurements of S parameters: 9 kHz – 10 MHz

Surface current measurement: 9 KHz – 1 MHz

Study of the behaviour of materials and joints when subjected to lightning strikes

MHPress

Measurement of electromagnetic shielding effectiveness (SE) according to ASTM D4935

DC frame resistance measurement

HPC computing cluster

HPC cluster with 22 machines, each with 2 Xeon E5-2680 v3 @ 2.50 GHz computing processing units with 24 cores

2 display machines, each with 2 Xeon E5-2660 v3 @ 2.60 GHz computing units with 20 cores

1 workstation with 2 Intel Xeon 5220R 2.2 GHz computing units with 24 cores

Ensayo de antena NAVANT/GALILEO

NAVANT/GALILEO antenna testing in compact field (AIRBUS DS)

Ensayo en BIANCHA

Aeronautical radome testing at BIANCHA

Medida de firma radar en campo compacto (AERTEC)

UAV radar signature measurement in compact field (AERTEC)

Medida de firma radar de UCAV del Grupo STO-OTAN

Radar signature measurement in compact UCAV field by the STO-NATO TG-329 Group on ‘Radar Signature Measurement & Validation of a UCAV’