TYⅠ 6U Core Platform satellite

The illustration to the right is of the TYI satellite design to launch four time in 2018.


Its design is based on the following selections:

6U Core Platform Package

Fine ACS & ADS:

GPS

S-band communication

Deployable panel

Inter-satellite link  (optional)

Propulsion (optional)


The satellite provides the following key resources to these payloads:

Payload volume: >3U

Average availble power for payloads: 10W

Pointing performance: 0.1-0.5 degrees

Downlink per day: 4G B (1 ground station, SSO orbit)

TYⅡ 27U Platform

The illustration to the right is of a 27U configuration. Its design is based on the following selections:

27U Core Platform Package

Fine ACS & ADS

GPS

S-band communication

Inter-satellite link  (optional)

Propulsion (optional)

Double Deployable panel

A 27U platform with this or a similar configuration can support many operational missions with demanding requirements e.g. intensive communication or remote sensing types of missions.

The satellite provides the following key resources to these payloads:

Payload volume: 20U+

Average available power for payloads: 10W (no deploable panels), 30W (1 dep. panel) & 50W (2 dep. panels)

Pointing performance: 0.1 degrees

Downlink per day: 6 GB (1 ground station, SSO orbit)