SELENE

විකිපීඩියා, නිදහස් විශ්වකෝෂය වෙතින්
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Kaguya
Selene.gif
Mission type Lunar orbiter
Operator JAXA
COSPAR ID 2007-039A
SATCAT no. 32054
Spacecraft properties
Manufacturer NEC Toshiba Space Systems
Launch mass 2,914 kilograms (6,424 lb)
Power 3,486 watts
Start of mission
Launch date 14 September 2007, 01:31:01 (14 September 2007, 01:31:01) UTC
Rocket H-IIA 2022 F13
Launch site Tanegashima Yoshinobu 1
Contractor Mitsubishi
End of mission
Decay date 10 June 2009, 18:25 (2009-06-10UTC18:26Z) UTC
Orbital parameters
Reference system Selenocentric
Periselene 100 kilometres (62 mi)
Aposelene 100 kilometres (62 mi)
Inclination 90 degrees
Period 2 hours
Lunar orbiter
Orbital insertion 3 October 2007
Instruments
  • X-ray Spectrometer (XRS)
  • Gamma Ray Spectrometer (GRS)
  • Multi-band Imager (MI)
  • Spectral Profiler (SP)
  • Terrain Camera (TC)
  • Lunar Radar Sounder (LRS)
  • Laser Altimeter (LALT)
  • Lunar Magnetometer (LMAG)
  • Charged Particle Spectrometer (CPS)
  • Plasma energy Angle and Composition Experiment (PACE)
  • Radio Science (RS)
  • Upper-atmosphere and Plasma Imager (UPI)
  • Relay Satellite aboard Okina (RSAT)
  • VLBI Radio source aboard Okina and Ouna (VRAD)
  • High Definition Television cameras (HDTV)

SELENE (/ˈsɛln/; Selenological and Engineering Explorer), යනු ජපානයේ ප්‍රකට ලෙස කගුයා (かぐや?) (ඉංග්‍රීසි:  Kaguya) ලෙස හැඳින්වෙන චන්ද්‍ර කක්ෂයේ සිට නිරීක්ශණය කරන යානයකි.

ආශ්‍රිත[සංස්කරණය]

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