MIPS(Miniature Ion Propulsion System)

MIPS(Miniature Ion Propulsion System)

Vendor: NeSTRA
Shipping:
12 months
¥30,000,000
Miniature Ion Propulsion System for 50 kg class microsatellite
  • Dimensions:
    390 × 280 × 160 mm
    Mass:
    6㎏ (incl.1kg of Xe propellant)
    Power Consumption:
    30 W
    Specific Impulse:
    1200 s
    Total Impulse:
    12000 Ns
    Total Velocity:
    240 m/s (for 50 kg microsatellite)
    Ion Thruster Unit:
    Ion Source + Nuetralizer
    Thrust:
    0.3 mN
    1. Satellite
    2. Year
    3. Developer
    4. Inclination (deg)
    5. Altitude (km)
    Satellite: HODOYOSHI-4
    Year: 2014
    Developer: The University of Tokyo
    Inclination (deg):97
    Altitude (km):620
    Satellite: PROCYON
    Year: 2014
    Developer: JAXA/The University of Tokyo
    Inclination (deg):
    Altitude (km):

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