The Spacecraft


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A spacecraft or artificial satellite can be comprised of eight hardware subsystems: Command & Data Handing (C&DH), Electrical Power System (EPS), Guidance, Navigation, & Control (GN&C), Structures (STRUCT), Mechanisms (MECH), Telemetry, Tracking, & Command (TT&C), Thermal Control, Payload, and Propulsion. Non-hardware subsystems include Flight Software, an Orbital Analysis team, a Mission Operations Center (MOC), and a Ground Control Station (GCS). ABEX does not feature propulsion and includes particle radiation analysis within the Thermal Control team. Let's learn more about the ABEX subsystems.

Subsystem Teams

Structural Integrity

Auburn University - Dr. Russell Mailen

Command & Data Handling

University of Alabama - Dr. Patrick Kung

Electrical Power System

University of Alabama - Dr Jaber Abu Qahouq

Guidance, Navigation & Control

University of South Alabama - Dr. Carlos Montalvo

Mechanisms

Auburn University - Dr. Russell Mailen

Telemetry, Tracking & Command

University of South Alabama - Dr. Saeed Latif

Thermal Control

Auburn University - Dr. Nicholas Tsolas

Flight Software

Auburn University - Dr. Xiao Qin

Payload

University of Alabama in Huntsville - Dr. L. Dale Thomas

Particle Radiation

Auburn University - Dr. Nicholas Tsolas

Astrodynamics

Auburn University - Dr. Davide Guzzeti

Project Management

University of Alabama in Huntsville - Dr. L. Dale Thomas

Systems Engineering

University of Alabama in Huntsville - Dr. L. Dale Thomas

Mission Operations Center

University of Alabama in Huntsville - N/A

System Integration

University of Alabama in Huntsville - Dr. L. Dale Thomas


In Partnership With

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University of Alabama Birmingham Logo
Alabama Space Grant Consortium Logo
University of Alabama Huntsville Logo
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