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High-Rate Data Recorder
Design a low cost, compact, solid-state data recorder for suborbital vehicles. The recorder will have a 45 GB minimum capacity and a record rate of at least 400... -
Communication System and Avionics for Deployable Small Free Flying Payloads
This IRAD will develop a core part of the communication system for the small free flying payloads. In particular, this portion of the system will consist of the circuitry... -
Cubesat Fine Sun Sensor
A second generation Wallops Fine Sun Sensor (WFSS) was developed as a 2016 IRAD project. The project for 2017 will be to assess the need for radiation hardening and complete... -
CubeSat Modular Deployable Solar Arrays
Advanced CubeSat missions have demanding power requirements relative to their limited available surface area that drive the need for deployable solar arrays. Vendors have not...