About Communications and Broadcasting Engineering Test Satellites "Kakehashi" (COMETS)
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Kakehashi(COMETS), a two-ton geostationary three-axis stabilized satellite, is being created to develop the new technologies required for future fields in communications and broadcasting. Relay satellites in geostationary orbit will be used to develop the following technologies: |
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Major Characteristics
Launch Date | 2/21/1998 |
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Launch Vehicle | H-II Launch Vehicle (5F) |
Launch Site | Tanegashima Space Center |
Weight | 3.9t at lift-off, 2t at Initial geostationary stage |
Orbit | Geostationary orbit 121deg. E. Iongitude |
Configuration | Structure: 2m×3m×3m Box shape, Solar paddle: 3m×15m (cantilever) |
Design Life | 3 years |
Power | GaAs Solar Cell - Flexible Solar Paddle: Approx. 5.3kW(EOL) NNiH2 Battery DOD≥70% |
Attitude Control | Three-axis stabilized Controlled bias momentum type |
Unified Propulsion | 1700N Apogee kick engine NTO, N2H4-Bi-propellant 50N Thruster×4 1 N Thruster×8 (redundant) N2H4-mono-propellant |