COTS Boards
ATE & Test Systems
- - Avionics Suite Tester
- - BrahMos Checkout
- - Digital Flight Control Computer
- - Go No Go testers
- - Power Module Tester
- - Generic RF ATE
- - Cable Harness Test System
- - Bus Management Unit
- - Count Down Test System
- - INTU ATE
- - Redundant Strap Down INS ATE
- - Scan Mirror Test
- - Strain Data Acquisition System
- - Laser Guided Bomb Tester
Identify Friend & Foe
- - STANAG
Space Systems
Software & Application Products
RF & Microwave
Electronic Warfare
Cockpit & Rugged Displays
Radar and Radar Subsystems
Avionic Systems
Laser and Electro Optic System
Power Supply
Naval Systems
Communication Products
Gimbal and Actuator Controller Products
Launch and Fire Control Systems
High Speed Processors
Digital IF Processors & Waveform generators
Console
Navigation System
During operational period, the satellite must cope with a volatile external environment. A spacecraft must endure deep space, solar/ planetary flux and internal heat among other factors.
The components used in the satellite have a limit on their operating temperature. Any operation beyond these limits may deteriorate the performance of the system or subsystems. It is thus essential to keep the components within their working temperatures. Thus the aim is to ensure smaller thermal gradients and little to no thermal stress across the components / structures.
A thermal control system of a spacecraft can be implemented in two ways
• A Passive Thermal control System with MLI sheets, OSR and surface coatings as key components.
• An Active Thermal Control System using electric heaters and heat pipes.
Active or Passive, Data Patterns is equipped to tailor design solutions for varied thermal management challenges.