Satellite Laser Ranging and Velocity Measurement System of Spacecraft
A laser ranging and velocity measurement system designed for spacecraft, enabling automatic docking by precisely measuring mutual arrangement parameters.
Key figurescomparable across the catalogue
- Mass
- 2 kg
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Purpose
- Measuring of mutual spacecraft arrangement parameters for automatical docking.
- Year of release
- 2020
- Design life
- It will be determined according to development result.
- Lead time
- According to specified hardware components based on development result.
- Flight qualification of the product
- No
- Possibility to adapt the product to customer requirements
- Yes
- Maximum range
- 100-300 m
- Range error
- 10-100 mm
- Velocity error
- 1-10 mm/sec.
- Field of view
- 5° kh 5° - 30° kh 30°
- Mass
- 2-4 kg
- Operating wave length
- 1550 nm
About
The Satellite Laser Ranging and Velocity Measurement System of Spacecraft is engineered to measure the mutual arrangement parameters of spacecraft, facilitating automatic docking procedures. It determines distance by analyzing the delay of a reflected laser beam and measures velocity using the Doppler frequency shift of an optical carrier. The system is also capable of receiving a 3D image of an object or a part of it. Released in 2020, its guaranteed service life and estimated production/delivery time are determined based on development results. While it currently lacks flight qualification, it offers the possibility of adaptation to customer requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.