The SINOD-D (SRI International NanoSat Orbital Demonstration) series of 2U CubeSats are technology demonstration satellites developed by SRI International.
The satellites were provided by Tyvak Nano-Satellite Systems Inc.
One of the technologies demonstrated on these satellites is a high-speed data downlink for wide-bandwidth CubeSat payloads via software defined radio communications. No further details are know.
Nation: | USA |
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Type / Application: | Technology |
Operator: | SRI International |
Contractors: | SRI International (prime); Tyvak Nano-Satellite Systems Inc. (bus) |
Equipment: | |
Configuration: | CubeSat (2U) |
Propulsion: | None |
Power: | Solar cells, batteries |
Lifetime: | |
Mass: | 2 kg |
Orbit: | 494 km × 800 km, 64.78° (#1, 3) |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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SINOD-D 1 | 2015-058L | 08.10.2015 | Va SLC-3E | Atlas-5(401) | with Intruder 11A, Intruder 11B, SNaP-3 ALICE, SNaP-3 EDDIE, SNaP-3 JIMI, LMRSTSat, SINOD-D 3, AeroCube 5C, OCSD A, ARC 1, BisonSat, Fox 1A, PropCube 1, PropCube 3 | |
SINOD-D 2 | - | with ? | ||||
SINOD-D 3 | 2015-058P | 08.10.2015 | Va SLC-3E | Atlas-5(401) | with Intruder 11A, Intruder 11B, SNaP-3 ALICE, SNaP-3 EDDIE, SNaP-3 JIMI, LMRSTSat, SINOD-D 1, AeroCube 5C, OCSD A, ARC 1, BisonSat, Fox 1A, PropCube 1, PropCube 3 |