Phoenix
Flight Computer
Technical Specifications
| Microprocessor | LEON3 SparcV8 | |
| Flash | 0.064 | Gb |
| SDRAM | 0.128 | Gb |
| Clock Frequency | 50.0 | MHz |
| Supply Voltage | 5.0 - 15.0 | V |
| Operating Temperature | -30.0 - 65.0 | °C |
Overview
L3Harris’ Phoenix is a modular and scalable ruggedized flight computer designed for use in a number of launch vehicle and spacecraft applications such as launch vehicle guidance, navigation and control (GNC), launch vehicle engine control, satellite attitude control, mission data network control (solid-state compressive recorder), instrumentation & display controller, software defined radio controller, vehicle health & status monitoring, command & data handling computer and payload control computer.