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A Victim of Our Own Success
Long overdue update on Holoseat... V0.2 works so well that we got sidetracked using the prototypes instead of continuing development. But, development is underway again with some great new ideas and a first public demo.
Ground Sphere CubeSat Ground Station:
Update for LNA production
The 20dB gain LNA (Low Noise Amplifier) is critical to the receive sensitivity of Ground Sphere, making the difference between a trace of a signal and AX-25 decode.
Open Source Lidar (07/06/2015 03:56 am)
The idea of this project is the conceptual development of a modularized open source lidar system. The
possibility of realizing an open source lidar system should be evaluated by defining a modularized
framework with interface definitions. The goal of this modularized open lidar system is to have a...
- OBI (04/06/2015 03:18 am)
Mathematics Tool Kit (01/22/2015 09:09 pm)
Yavin Thruster (01/17/2015 06:55 pm)
Welcome to Mach 30's Yavin Thruster project. If you have ever wondered what makes rockets work or how engineers go about designing rocket engines, then this is the project for you. We are going to demonstrate how you can go from requirements to analysis and conceptual design (1) to detailed design (2) to manufacture (3) and ultimately test....
High Altitude Rocket Project (HARP) (10/02/2014 10:29 am)
A community based effort to develop, design, build and fly a rocket capable of reaching the Stratosphere and returning to earth in whole, or in part as a glider. The glider and/or booster are to have onboard telemetry, First Person Video (FPV) and OSD capabilities to transmit live video and data as well as autonomously fly back in close proximity to either the launch point or a designated landing area based on GPS coordinates. The glider should be able to loiter over an area for an extended period of time (1 or more hours) power-pack permitting by gently spiraling down and riding thermals or deploying a small electric motor turning a folding propeller. The glider, when providing FPV and OSD data should also optionally be R/C controllable by a human operator during the final 300-400 feet of descent to landing....