Image of Jena-Optronik GmbH - Astro APS on the satsearch marketplace

Key highlights

ASTRO APS is an autonomous star sensor with the most advanced radiation hard CMOS Active Pixel Sensor (APS) detector technology.

A single box design has been chosen with minimized dimensions, low mass and low power consumption while maximizing the ease of integration on the spacecraft. ASTRO APS shows high reliability and radiation hardness by careful selection of EEE Parts, reduced number of components and special software algorithms to cope with radiation events.

The technical key parameters of the APS based star sensor are the low mass budget with approx. 2kg, the low power consumption with approx. 5W and the attitude quaternion accuracy of <1arcsec (1sigma). These data define a new level of compactness compared to CCD-based star sensors for the GEO telecom market (>18 years life time, <25 years radiation robustness for GEO missions).

The improvements in dimensions and performance are realized with the replacement of the CCD detector by the APS detector technology. The mass and envelope benefit is based on the very high functional integration of the APS detectors. The whole analogue read-out and sampling electronics is placed on the detector chip. This saves PCB area compared to CCD-based systems. The parts count for an APS based star sensor is reduced accordingly. Along with that, the unit costs are reduced and the system reliability is increased.

Manufacturing

The ASTRO APS make use of Acktar coatings for thermal management and stray light suppresion.

Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.

Last updated: 2024-07-29

Image of Jena-Optronik GmbH - Astro APS on the satsearch marketplace

Downloads

Technical specs

power consumption
RS422: < 11 W, Peltier Cooler ON max
RS422: < 5 W, Peltier Cooler OFF
MIL-STD-1553B < 12 W, Peltier Cooler ON max
MIL-STD-1553B: < 6 W, Peltier Cooler OFF
voltage
100V nominal (other voltages on demand)
50V nominal (primary power s/c bus architectures)
28 V nominal (optional selectable for either regulated or unregulated)
data interface
RS422
MIL-STD-1553B
sun exclusion angle
26 deg
slew rate
< 0.3 deg s^-1
attitude knowledge about boresight
< 8 arcsec
attitude knowledge cross boresight
< 1 arcsec
non-operating temperature
-40 to 70 C
operating temperature
-30 to 60 C
field of view
20 deg
height
154 mm
length
237 mm
width
154 mm
mass
approx. 2 kg (including baffle, GEO-shielding, DC/DC-converter, MIL1553)

Export

  • Click here to add the Jena-Optronik GmbH - Astro APS to the Valispace engineering tool from satsearch
  • Click here to add the Jena-Optronik GmbH - Astro APS to Lynapse Studio by Spacebackend
  • Click here to add the Jena-Optronik GmbH - Astro APS to 360 by IENAI

from our blog

Go to blog

Star trackers: the cutting edge celestial navigation products available on the global space marketplace

Sun sensors - an overview of systems available on the global marketplace for space

Reaction wheels: an overview of attitude control systems available on the global marketplace for space