Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

SINOD-D 1, 2, 3

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
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
SINOD-D 1 2015-058L 08.10.2015 Va SLC-3E Atlas-5(401) with Intruder 13, Intruder 14, 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 13, Intruder 14, 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

References:

Cite this page: