2006-041A
ISAS SOLAR-B was launched on the final M-5 in 2006. It was named Hinode ('Rising Sun') and carried optical and X-ray solar telescopes. The satellite involved NASA's participation under the Solar-Terrestrial Probe series of the Sun-Earth Connection theme, with an optical instrument package developed by Lockheed's Palo Alto solar group and an X-ray telescope developed by Lockheed and the Smithsonian Astrophysical Observatory. The SOLAR-B satellite was built by MELCO.
The 0.5-meter SOT has a resolution of less than 0.1 arcsec across a few-arcmin field of view; the EIS and XRT reach 1 arcsecond with a much larger field 1/2 degree field of view.
The M-V-7 has a launch mass of 140t. It carried subsatellites HIT-SAT and SSSAT.
Hinode's Mass is 900 kg. Box + 2 panels, span is 10.3m. Size is 1.6m x 3.8m.
A - payload B - solid C - slow decay after 2 days D - rapid decay E - slow decay F - payload Gslow Hslow Jmed K
| SOLAR B | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2006 Sep 22 | 2136 | Launch by M-V-7 | USC |
| T+1:15 St 1 sep | |||
| T+1:15 St 2 burn, 140 km | |||
| T+3:06 Fairing sep | |||
| T+3:20 St 2 sep | |||
| T+3:22 St 3 nozzle extension | |||
| T+3:25 St 3 burn | |||
| 2141 | T+5:11 St 3 burnout, 300 km | ||
| T+5:47 Begin reorientation | |||
| T+6:40 End reorientation | |||
| 2144 | T+8:30 Stage 3 sep | ||
| 2149 | T+13:50 HIT-SAT sep | ||
| 2152 | T+16:30 SSSAT sep | ||
| 2209 | T+33:30 Solar panels deploy | ||
| 2006 Sep 22 | 94.11 271 x 678 x 98.3 | ||
| 2006 Sep 25 | TCM-1 | 94.54 318 x 674 x 98.3 | |
| 2006 Sep 27 | TCM-2 | 96.24 482 x 674 x 98.3 | |
| 2006 Oct 2 | TCM-3 | 98.44 674 x 694 x 98.1 | |
| 2006 Oct 23 | 98.45 674 x 695 x 98.1 | ||
Payload:
- SOT 0.5m solar optical telescope
- FPIP NASA/ Lockheed-Palo-Alto focal plane instrument package for optical telescope
- BFI broadband filter imager
- NFI narrowband filter imager
- SP spectropolarimeter
- XRT Solar-B XR telescope for coronal studies. (Golub/SAO) 0.35m aperture single-shell Wolter II.
- EIS EUV imaging spectrometer
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