
TechEdSat 15 (TES 15) [NASA]
The TechEdSat 15 (TES 15) is a 3U CubeSat from NASAs Ames Research Center in Californias Silicon Valley, which will be used to test several technologies.
This three-unit CubeSat weighs 9.1 pounds and carries experiments that are being advanced in TechEdSats Nano-Orbital Workshop (NOW) rapid flight development series.
TechEdSat-15s primary experiment is a version of an exo-brake intended to survive much higher temperature environments several hundred degrees than in previous flights. It will demonstrate the next step forward in nanosatellites ability to target an Earth entry point. The exo-brake is a device that applies drag in Earths exosphere the uppermost reaches of the atmosphere to slow the speed of a satellites descent and change its direction. This experiment will permit the satellite to survive closer-to-peak heating, maintain telemetry, and assess the dynamics as the system enters the top of the atmosphere.
Another experiment on TechEdSat-15 includes the Beacon And Memory Board Interface (BAMBI), which optimizes internal and external data transfer from the nanosatellite.
The TechEdSat-NOW series has multiple research goals including using the exo-brake to de-orbit high-altitude nanosatellites at end of mission to reduce issues related to orbital debris. Additionally, drag modulation has uses for sample return from low-Earth orbit as well as tailoring orbits during aero-pass maneuvers for future planetary applications. The TechEdSat-15 project is managed by Ames and funded by the Ames Engineering Directorate. TechEdSat-15 partners include San Jose State University.
TechEdSat-15 was launched on the second Firefly-Alpha (Block 1) rocket and reached orbit, although lower than planned.
| Nation: | USA |
|---|---|
| Type / Application: | Technology, education |
| Operator: | NASA Ames Research Center |
| Contractors: | NASA Ames Research Center |
| Equipment: | |
| Configuration: | CubeSat (3U) |
| Propulsion: | None |
| Power: | Solar cells, batteries |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| TechEdSat 15 (TES 15) | 2022-122C ? | 01.10.2022 | Va SLC-2W | p | Firefly-Alpha (Block 1) | with Serenity (2), GENESIS G, GENESIS J, Qubik 3, Qubik 4, FossaSat 1b (2), Firefly Capsule 2 |

Further TechEdSat missions:
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