TechEdSat 5 (TES 5) (original) (raw)
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.
TechEdSat 5 [NASA]
TechEdSat 5 (Technical and Educational Satellite 5) is a 3.5U CubeSat. It was built as a conjoined project between San Jose State University (SJSU) and the University of Idaho as a collaborative engineering project, with oversight from the NASA Ames Research Center.
The TechEdSat-5 satelliteis based on the TechEdSat-4 design, but using an enlarged 3.5U CubeSat bus. It will introduce a modulating exo-brake capable of changing its surface area allowing the satellite to more precisely enter the atmosphere.
TechEdSat 5 has following science and mission objectives:
- Establish improved uncertainty analysis for eventual controlled flight through the Thermosphere (perform detailed comparison to the TES-3 and TES-4 with respect to key Thermosphere variable uncertainty).
- Improve prediction of re-entry location.
- Provide the base technology for sample return technology from orbital platforms.
- Provide the eventual testing of independent TDRV-based planetary missions
- Provide engineering data for an On-Orbit Tracking Device that could improve the prediction of jettisoned material from the ISS.
The satellite was launched on board of HTV 6 on an H-2B-304 rocket to be delivered to the International Space Station, from where it will be deployed at a later date.
Nation: | USA |
---|---|
Type / Application: | Technology, education |
Operator: | SJSU, University of Idaho, NASA Ames Research Center |
Contractors: | SJSU, University of Idaho, NASA Ames Research Center |
Equipment: | Modulated Exo-Brake |
Configuration: | CubeSat (3.5U) |
Propulsion: | None |
Power: | Solar cells, batteries |
Lifetime: | 10 days |
Mass: | 4 kg |
Orbit: | 397 km × 408 km, 51.64� |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks |
---|---|---|---|---|---|
TechEdSat 5 (TES 5) | 1998-067LB | 09.12.2016 | Ta YLP-2 | H-2B-304 | with EDT, TechEdSat 5, EGG, TuPOD, AOBA-VELOX 3, STARS C, FREEDOM, ITF 2, Waseda-SAT 3, OSNSAT, Tancredo 1 |