Dual Horizon Crossing Indicator
Overview
The Dual Horizon Crossing Indicator (HCI) is a single assembly that contains two Pyroelectric Optical Barrel Assemblies and pulse conditioning circuitry. It is designed to operate at GEO orbit and used during transfer orbit for satellite spin rates of from 2 RPM to 60 RPM. Each HCI has a 1.5 degree beam width and the separation between the two HCI’s is 10 degrees. The output from each of the HCI’s is an analog pulse whose pulse width is equivalent to the Earth chord length and provides a single leading edge and trailing edge threshold crossing corresponding to the Space/Earth crossing and the Earth/Space crossing. The common chassis mounting of the two heads and the sharing of some common electronics provides for a compact lightweight assembly. A common alignment mirror is provided.
Looking for more information or want to purchase?
Overview
- Name
- Dual Horizon Crossing Indicator
- Vendor
- Servo
- Subsystem
- ACDS Subsystem
- Component Type
- Earth/Horizon Sensor
- Form Factor
- SmallSat
- Heritage
- N/A
Vendor Details
- Name
- Servo
- Website
- https://www.servo.com/
- Founded
- 1984
Vendor Request for Information Form
Specifications
- Subsystem
- ACDS Subsystem
- Component Type
- Earth/Horizon Sensor
- Form Factor
- SmallSat
- Vendor
- Servo
- Dry Mass
- 0.8 kg
- Average Power
- 2.0 W
- Heritage
- N/A
- Status
- In Production
Try Designer
Design, model, and evaluate satellite mission concepts quickly with our software.
Servo
View all products