Telemetry is concerned with the problem of making automatic, real-time measurements of remote data which are transmitted to base stations for further analysis. We present here an overview of our work in rocket telemetry for a Stage II Rocket which focuses on problems related to real-time telemetric data acquisition from high-speed, high-altitude projectiles, with detailed overviews of contributions from the six student teams, including: Airframe Team, Propulsion Team, Software, Sensors and Acquisition Team, Computational Physics Team, Launch and Recovery Team and the Computer Modeling Team. The Airframe Team designs the mounting apparatuses for the interior of the rocket. Our Propulsion Team synthesized and thrust tested the fuel we will use for rocket propellant, which is comprised of (Ammonium Nitrate-Oxidizer), C12H22O11 (Sucrose[Sugar]-Fuel) and HTPB(Hydroxyl-Terminated Polybutadiene- Fuel and Binder). The Software, Sensors and Acquisition Team is responsible for designing and programming the scientific equipment that will be onboard the rocket (Steering fins, an Arduino Microcontroller and a Two-Axis Accelerometer to maintain a linear flight path). Our data will be video, 3 axis acceleration, tilt, and altitude. The Computational Physics Team derived models to predict the rockets performance and they worked with the Computer Modeling Team to make CAD sketches. The Launch and Recovery Team make sure we follow safety precautions in launch and will use GPS tracking to retrieve the rocket when landed. The broader goal of this project is to recruit and invigorate future scientists at community colleges specializing in aerospace studies by providing a basic starting point from which they can learn and on which they can improve. We expect that by sharing our initial discoveries and experiences this multi-disciplinary research project, we will help to encourage other students at community colleges to actively participate in realistic team aerospace projects at an earlier stage in their educations.