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FORMOSAT 5

FORMOSAT 5 [NSPO]

NSPO started FORMOSAT 5, the first Remote Sensing Program, for the Second Phase Space Program (2004~2018). The program emphasizes on building up the capabilities for independent development of spacecraft and payload instruments. Being the prime contractor for the Formosat-5 system, NSPO takes the sole responsibility of all development phases.

The strategy for the program is to acquire key technology and setup a heritage bus design for NSPO. The key technology to be developed by NSPO includes flight software, EGSE and IPS. Additionally, NSPO and domestic partners will jointly develop some other key components, such as CDMU and PCDU. In the meantime, another goal for the Formosat-5 is to build-up the capability for the high-resolution optical remote sensing instrument by integrating NSPO with the ITRC (Instrument Technology Research Center) of NARL.

The objectives of the mission are as follows:

  1. To develop a spacecraft bus platform and establish optical instrument capability by integrating the domestic R&D resources.
  2. To conduct leading space science missions.
  3. To utilize remote sensing technology for the applications of disaster mitigation and environment monitoring.
  4. To last supply of remote sensing images for the users of FORMOSAT-2.

Formosat-5 has an optical payload and a number of science payloads. The optical payload, Remote Sensing Instrument (RSI), will be jointly developed by ITRC and NSPO under support of domestic contractors. Its strategy is to establish capabilities of system design, integration & test, opto-mechanical system calibration and developing key component development for the RSI at the first stage so that the goal of self-reliant RSI can be accomplished at the next program. (Resolution: (1) Pan 2 m, (2) MS 4 m, Swath: 24 km)

Additional scientific payloads are:

  • Magnetic Field Instrument (MFI)
  • Marine Data Relay Payload (MDRP)
  • New payload(To be announced soon)
Nation: Taiwan (Republic of China)
Type / Application: Earth observing
Operator: NSPO
Contractors:
Equipment:
Configuration:
Propulsion:
Power: Solar cells, batteries
Lifetime: 5 years
Mass: 525 kg
Orbit: 720 km SSO
Satellite COSPAR Date LS Launch Vehicle Remarks
FORMOSAT 5 - 2017 Va SLC-4E Falcon-9 v1.2 with ?

References:

  • NSPO website