The e-POP payload consists of eight scientific instruments that will aid in reaching the project's scientific goals:
Instrument | Description | PI | Scientific Output |
---|---|---|---|
CER | Coherent EM Radio Tomography | Bernhardt | Electron content |
FAI | Fast Auroral Imager | Cogger | Infrared and visible images |
GAP | GPS Attitude and Profiling Experiment | Langley | Spacecraft position and attitude |
IRM | Imaging and Rapid-Scanning Ion Mass Spectrometer | Yau | Low energy ion detection |
MGF | Fluxgate Magnetometer | Wallis | 3-D magnetic field and currents |
NMS | Neutral Mass Spectrometer | Hayakawa | 0.1-2km/s neutral particles |
RRI | Radio Receiver Instrument | James | Radio wave propagation |
SEI | Suprathermal Electron Imager | Knudsen | Low energy electron detection |
The e-POP instruments will be supported by Cascade, the companion commercial payload on CASSIOPE, which permits the on-board storage of up to 75 GB of e-POP data. This data can be downlinked to the ground at a rate of over 300 Mbits/s, allowing the e-POP payload to capture up to 15 GB per day of valuable scientific data.
The animation below shows the simulated orbit trajectory of one day of e-POP operation (14 orbits). The payload will be able to sample a large set of local times, and all latitudes below 80°.
©2013 Institute for Space Imaging Science