F-1 (satellite)
Flight Model of F-1
|
|
| Mission type | Education Technology |
|---|---|
| Operator | FPT/ASTC |
| Mission duration | Failed to contact ground |
| Spacecraft properties | |
| Spacecraft type | 1U CubeSat |
| Launch mass | 1 kilogram (2.2 lb) |
| Start of mission | |
| Launch date | 21 July 2012, 02:06 UTC |
| Rocket | H-IIB |
| Launch site | Tanegashima Y2 |
| Deployed from | ISS |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Inclination | 51.65 degrees |
F-1 is a 1U CubeSat built by FSpace laboratory at FPT University in Vietnam, in partnership with Angstrom Space Technology Center (ASTC), Uppsala University and NanoRacks LLC. Its mission is to train young engineers and students about aerospace engineering and evaluate an advanced 3-axis magnetometer (SDTM) designed in Sweden by ASTC.
F-1 was launched on 21 July 2012 and delivered to International Space Station (ISS) aboard Kounotori 3 along with the Raiko, We Wish, Niwaka and TechEdSat cubesats. Then, on October 4, 2012, it was deployed into orbit from ISS using JEM Small Satellite Orbital Deployer (J-SSOD) which was attached to the Kibo module's robotic arm. As of November 2, 2012, F-1 failed to confirm communication after the orbital deployment.
1. Backup UHF channel (only operational in daylight):
Pulse-Width-Modulation Morse code telemetry beacon
2. Main VHF channel (operational during night time but may be turned on in daylight later)
F-1’s KISS packet format
Note:
...
Wikipedia