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Tenma
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Tenma
Tenma (Japanese for "Pegasus")
NamesASTRO-B
Mission typeX-ray astronomy
OperatorISAS
COSPAR ID1983-011A Edit this at Wikidata
SATCAT no.13829
Mission duration5 years, 9 months, 27 days
Spacecraft properties
Launch mass216 kg (476 lb)[1]
Dimensions0.94 m × 0.895 m (3.08 ft × 2.94 ft)
Start of mission
Launch date20 February 1983, 05:10 UTC
RocketM-3S
Launch siteKagoshima Space Center
End of mission
DisposalDecommissioned
Last contact17 December 1988[2]
Decay date19 January 1989
Orbital parameters
Reference systemGeocentric[1]
RegimeLow Earth
Perigee altitude489 km (304 mi)
Apogee altitude503 km (313 mi)
Inclination31.5°
Period94 minutes
← Hinotori (ASTRO-A)
Ginga (ASTRO-C) →

Tenma, known as ASTRO-B before launch, was a Japanese X-ray astronomy satellite developed by the Institute of Space and Astronautical Science. It was launched on 20 February 1983, using a M-3S rocket on the M-3S-3 mission. It was the second X-ray observatory successfully operated by Japan after Hakucho (CORSA-B),[3][a] and it had a superior temporal and spectral sensitivity compared to its predecessor.[5]

Battery failure in July 1984 caused the operation to become limited, and continuing problems lead to the termination of X-ray observation on 11 November 1985,[6] however it remained in sporadic contact until 17 December 1988.[2] It reentered the atmosphere on 19 January 1989.[b]

Highlights

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  • Discovery of the iron helium-like emission from the galactic ridge.[6]
  • Iron line discovery and/or study in many LMXRB, HMXRB and AGN.[2]
  • Discovery of an absorption line at 4 keV in the X1636-536 Burst spectra.

References

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