CSIP is a 3U CubeSat developed by the Air Force Research Laboratory/Space Vehicles Directorate (AFRL/RV).
CSIP was to be launched as a piggy-back payload on a Minotaur-1 from Wallops Island in June 2013, but was delayed to a later launch. The status is unknown.
| Nation: | USA |
|---|---|
| Type / Application: | Experimental |
| Operator: | Air Force Research Laboratory/Space Vehicles Directorate (AFRL/RV) |
| Contractors: | Air Force Research Laboratory/Space Vehicles Directorate (AFRL/RV) |
| Equipment: | |
| Configuration: | CubeSat (3U) |
| Propulsion: | |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| CSIP | - | with ? |
