NEXTAR

NEXTAR NX-300L
Manufacturer NEC Space Systems
Country of origin Japan
Applications Earth observation
Specifications
Spacecraft type Earth observation
Design life 3 to 5 years
Dry mass 250 kg (550 lb)
Payload capacity up to 250 kg (550 lb)
Dimensions 950 mm × 950 mm × 950 mm (37 in × 37 in × 37 in) (W×D×H)
Power Up to 600 W
Batteries Li-ion
Regime Low Earth orbit
Production
Status In Production

NEXTAR (from NEC Next Generation Star) is a Low Earth orbit Earth observation satellite bus designed and manufactured by NEC Space Systems of Japan.[1][2] This three axis stabilized platform has a bus dry mass of 250 kg (550 lb), it can carry payloads up to 250 kg (550 lb) and 600 W. It uses tri-junction GaAs has an expected life between 3 and 5 years.[1]

Its telemetry and control subsystem includes S band and X band channels.[1]

Platform models

As of 2014, there are three different models of the NEXTAR standardized platform. All feature a common core of features like using the SpaceWire communications protocol, the SpaceCube2 on-board computer and autonomous control functions. The different models are:[3]

List of satellites

Satellites using the NEXTAR platform.[1]


See also

References

  1. 1 2 3 4 "NEXTAR". NEC. Retrieved 2016-08-09.
  2. Wade, Mark. "NEXTAR NX-300L". Retrieved 2016-08-09.
  3. 1 2 3 4 Adachi, Masaki (July 2, 2014). "Introduction to NEC Space Business" (PDF). Space Systems Division NEC Corporation. Archived from the original (PDF) on 2016-08-31. Retrieved 2016-08-31.
  4. 1 2 3 Kallender-Umezu, Paul (November 24, 2014). "Japan's NEC Looks To Expand Commercial Market Footprint". Retrieved 2016-08-31.

External links

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