Small satellite calibration facility
The SSCF is designed to support UK and international start-ups and SMEs, offering rapid, affordable access to world-class calibration services. This lowers the barrier to entry for space missions and enhances the quality, reliability, and interoperability of Earth Observation (EO) data, supporting both commercial and scientific applications.
Access to facilities and systems
- Thermal vacuum environment with motion control stages for precise alignment of the customers instrument with the calibration sources
- Collimator for geometric characterisation.
- Blackbody sources for TIR radiometric calibration.
- STARWELL system, based on NPL’s STAR-cc-OGSE, enabling radiometric calibration from 320 nm to 2500 nm using monochromatic and broadband sources.
View systems specifications
Space Calibration Cryostat – Vacuum environment
- Provides thermal vacuum environment for customer’s instrument
-
Thermally controlled breadboard, design range -100°C to 80°C wider range possible please enquire. When instrument motion control stage fitted this limit the available temperature range.
-
Option to test in air and at room temperature.
-
Four 200mm diameter ports and two windows to view external calibration sources.
| Thermally controlled breadboard |
Range -100°C to 80°C |
|---|---|
| Options |
In air and at room temperature testing |
| Ports |
4 x 200mm plus 2 x windows to view external calibration sources |
Instrument motion control
- Rotation stage with hexapod to position device under test allowing optical axis alignment while under vacuum and selection of calibration sources.
-
Hexapod for fine positioning repeatability of 3.2 µrad in rotation, and 0.4 µm in displacement
-
Rotation stage for source selection, repeatability 0.34 mrad.
-
Motion possible over temperature range -20 ⁰C to +50 ⁰C, with a bake capability of +75 ⁰C (no motion).
| Hexapod repeatability |
3.2 µrad in rotation, and 0.4 µm in displacement |
|---|---|
| Rotation stage for source selection |
Repeatability 0.34 mrad |
| Temperature range |
-20 ⁰C to +50 ⁰C, with a bake capability of +75 ⁰C (no motion) |
Collimator – Geometric characterisation
- Image projection system with different targets for geometric characterisation of customer instruments Targets for MTF, PSD, MRTD characterisation. Custom targets available on request.
- 200mm aperture collimator system
- Vis/SWIR integrating sphere to illuminate object plane
- TIR Blackbody source operation from 0 to 125°C
- 0.5 to 20Hz chopper system
Blackbody – TIR radiometric calibration
- Temperature range 210K to 320K
- ITS-90 traceable source radiance uncertainty to better than 0.1K
- High emissivity ~0.998
- 200mm aperture – provision to stop target down with custom apertures.
- Heritage design, Based on ATSR/AATSR/SLSTR ground calibration targets – proven design with good performance
| Temperature range |
210K to 320K |
|---|---|
| ITS-90 traceable source radiance uncertainty |
0.04 – 2.10 W m-2 sr-1 |
| High emissivity |
~0.998 |
| Aperture |
< 0.03nm |
STAR-cc-OGSE
The SSCF also manages the traceable radiometric calibration in the UV-SWIR, initially using STAR-cc-OGSE which then led to the development of the new STARWELL facility.
Spectroscopically Tuneable Absolute Radiometric, calibration and characterisation, Optical Ground Support Equipment (STAR-cc-OGSE) was developed in partnership with the innovative company, M Squared. The STAR facility provides a state-of-the-art solution to instrument calibration and characterisation, ensuring the required performance is achieved while also minimising the time and effort involved in the pre-launch vacuum test environment.
MicroCarb, launched in 2025, was the first mission that used STAR-cc-OGSE. It is a joint mission between UKSA and CNES designed to measure sources and sinks of carbon, the principal greenhouse gas driving global warming.
STARWELL
Building on the knowledge gained from the development of SSCF’s STAR-cc-OGSE. STARWELL utilises much of the same science & engineering to enable quick turnaround, affordable access to radiometric calibration of small satellite payload instruments.
The SSCF system combines the design of the radiometric calibration setup from STAR-cc-OGSE with a novel SI-traceable reference detector and a 1 kHz pulsed tuneable laser. This enables radiometric calibration measurements from 320 nm to 2500 nm with both monochromatic and broadband sources. The sequence of images below show how the SSCF can scan through the visible spectrum using monochromatic radiation.
Small Satellite Calibration Facility offers a range of characterisations including:
- Absolute spectral response
- Linearity
- Polarisation sensitivity
- Spectral response function
- Stray light
- Spectral calibration
Small Satellite Calibration Facility Radiometric Specifications
|
Monochromatic spectral range |
320 nm – 2500 nm |
|
Monochromatic radiance |
0.04 – 2.10 W m-2 sr-1 |
|
Monochromatic tuning resolution |
< 0.01 nm |
|
Monochromatic wavelength accuracy |
< 0.03 nm |
|
Broadband spectral range |
300 nm – 2500 nm @ TCCT = 3080 K |
|
Broadband radiance |
2.0 W m-2 sr-1 nm(@1000 nm) |
|
Polarisation extinction ratio |
40 dB |
|
Reference detector absolute radiance calibration uncertainty |
< 0.5 % (k=1) |
