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Sun Sensors

77 Sun Sensors for Space Applications from 25 manufacturers listed on SatNow

Sun Sensors for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:Digital Sun Sensor for SmallSats
Satellite Type:
SmallSat, NanoSat
Segment:
Space
Type:
Digital Sun Sensor
Accuracy:
0.3 Degree (3-sigma)
Sun Field of View:
±60 Degree
Mass:
35 g
Radiation Tolerance:
100 krad (gamma)
Supply Voltage:
5 V
Interface:
UART, I2C, SPI, RS-422
more info
Description:An Analogue Quadrant Detector Fine Sun Sensor (FSS)
Satellite Type:
CubeSat
Segment:
Space
Type:
Analog Sun Sensor
Accuracy:
±0.3 Degree
Sun Field of View:
128 x 128 Degree(Nominal FOV), 138 x 138 Degree(Unobstructed FOV (To Be Free Of Straylight Sources)
Mass:
375 g
Radiation Tolerance:
10 krad
Supply Voltage:
0 to 5 V
Power Consumption:
0.25 W
Space Heritage:
Yes
more info
Description:Sun Sensor for LEO & GEO Orbits
Satellite Type:
SmallSat
Segment:
Space
Type:
Digital Sun Sensor
Accuracy:
0.5 Degree
Sun Field of View:
140 Degree
Update Rate:
10 Hz
Mass:
240 g
Supply Voltage:
12 to 50 V
Power Consumption:
50 mW
Interface:
RS-422, CAN, SPI
more info
Description:Indian Space Research Organisation (ISRO) is responsible for Design Development and production of electro-optic sensors and optics for spacecraft
Segment:
Space
Accuracy:
±5 Degree
Mass:
50 g
Space Heritage:
Yes
more info
Description:Three Analogue Fine Sun Sensors up to 114° FOV
Segment:
Space
Type:
Analog Sun Sensor
Accuracy:
±5 Degree
Sun Field of View:
Up to 114 Degree
Update Rate:
10 Hz
Mass:
With 3x Sensors: 102 gms, ±5 gms, Without Sensors: 87 g ±5 g
Radiation Tolerance:
20 krad
Supply Voltage:
5 V
Power Consumption:
185 mW
Space Heritage:
Yes
Interface:
RS-422
more info
Description:A CMOS-based fine sun sensor with a wide field of view & low power consumption
Satellite Type:
CubeSat
Segment:
Space
Accuracy:
0.2 Degree
Sun Field of View:
166 to 176 Degree
Update Rate:
Up to 2 Hz
Mass:
15 gms
Radiation Tolerance:
24 krad
Supply Voltage:
3.3 V
Power Consumption:
174 mW (Peak power)
Interface:
CAN, UART, RS-485, I2C
more info
Description:Analog Fine Sun Sensor for Telecom & Scientific Satellites
Segment:
Space
Accuracy:
0.15 Degee
Sun Field of View:
128 Degree
Mass:
650 g
Supply Voltage:
13 to 15 V
Power Consumption:
200 mW
more info
Description:Two Axes Solar Sensor based on an Active Pixel Sensor (APS) Detector
Segment:
Space
Type:
Analog Sun Sensor, Digital Sun Sensor
Accuracy:
±0.02 Degree
Sun Field of View:
128 x 128 Degree
Update Rate:
10 Hz
Mass:
330 g
Radiation Tolerance:
100 to 300 krad
Supply Voltage:
5 to 50 V
Power Consumption:
700 mW to 1 W
Space Heritage:
Yes
Interface:
RS-422
more info
Description:Fine Pointing High Accuracy Attitude Determination Sun Sensor
Segment:
Space
Accuracy:
±0.002 to 0.005 Degree
Sun Field of View:
4.25 x 4.25 Degree
Mass:
2030 g
Radiation Tolerance:
100 krad
Supply Voltage:
28 ±7 V
Space Heritage:
Yes
Interface:
RS-422
more info
Description:45 Degree Solar Sun Sensor from 6 to 36 V
Satellite Type:
SmallSat
Segment:
Space
Type:
Analog Sun Sensor
Accuracy:
±0.15 Degree
Sun Field of View:
45 Degree(line of sight)
Mass:
45 g
Supply Voltage:
6 to 36 V
Power Consumption:
0.4 W
Space Heritage:
Yes
Interface:
CAN
more info

What are Sun Sensors?

Sun sensors are navigational instruments that are used in space by a spacecraft to determine the direction and position of the sun to the position of the spacecraft. 

In a typical sun sensor, a thin slit is present at the top of a rectangular chamber which can be of different sizes and allows light to enter and fall on an array of photo detective cells at the bottom of the chamber. The chamber casts an image of a thin line on the chamber bottom. The cells at the bottom measure the distance of the image from a centerline and determine the refraction angle by using the chamber height.

Since these photo detective cells work on the principle of a photoelectric effect they convert the incoming photons into electrons and hence voltages which are in turn converted into a digital signal. When two sensors are placed perpendicular to each other, the direction of the sun about the sensor axes can be calculated. There are various types of sun sensors, each one best suited to the characteristics and requirements of the satellite.

Sun sensors are widely used in spacecraft attitude determination systems, orbit control, and attitude control of spacecraft. They are also used for solar array pointing, gyro updating, fail-safe recovery, meteorological systems, tracking systems, and navigation systems.



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