Mission Statement
ALL-STAR deliver a 3U CubeSat providing accesibility for on-board and on-orbit payload operations for one full year including tasks such as research, data collections, and test for future evolutions to the CubeSat structure in COSGC.
Objectives
- Create a reproducible modular bus
- Conform to the standard CubeSat Structure
- Create common payload interface
- Capable enough to be used for a variety of small research and technology based based payloads
- Built within six months of request after initial delivery in Spring 2012