Lunar Astronomy with the LUT on Chang’e-3
lander
National Astronomical Observatories, CAS/
Guangxi University
J. Wang on behalf of LUT group
Beijing
2018/12/07
Contents
 Lunar-based Ultraviolet Telescope
 Performance on the Moon
 Scientific results
The dreams to observe the Universe on the Moon
Far UV camera
with Appolo 16
 Lunar-based Ultraviolet Telescope (LUT, Cao+11)
 A small, but automatic, telescope aboard CE-3 working in NUV.
The FIRST automatic telescope landed on the extraterrestrial body in
mankind history.
 Scientific Objectives
– Monitoring variable stars
 Pulsating or binary stars, e.g., RR Lyr variables
 Variable stars in clusters
 Activities of solar-like stars
– Survey the sky
 Especially survey the low galactic latitude region;
 Violent flare stars
Lunar-based Ultraviolet Telescope I
 Milestones
– July 2004: Proposal Conception
– Feb. 2009: Project Approval
– Sep. 2009: Engineering Model
– Dec. 2011: Flight Model
– Dec. 02. 2013: Launch
– Dec. 16. 2013: First Light
– Jan. 2014 -- : Observations
– The FIRST automatic telescope on the
Moon for mankind.
LUT
First image
RA. 16:45:00
Dec 50:26:00
(Draco)
Lunar-based Ultraviolet Telescope II
Lunar Enterprise Daily,2015/01/01
A supporting system for LUT scientific obs
Exp vs S/N
Ins. setup
Finding chart & catalog
Obs sequence head
Obs sequence:
Time slot
Position of Gimbal
Rotation step
Target & comp coordinate
 Instrument Specifications
 Comp: Telescope+Pointing Reflector
Item Value
Diameter 150mm
Focal Length 562.5mm
Wavelength 245—340 nm
Field of view 1.36  1.36 Square Degrees
CCD camera E2V 47-20 UV enhanced
Working time lunar day time
Life time > one year
Weight 13.6 kg
Lunar-based Ultraviolet Telescope III
Performance on the Moon I
Sky Coverage: inside the red
circle Pointing calibration
Allow the telescope to point to any target &
trace smoothly
 Flux calibration
– ~13.5 mag in lunar day time
– ~15.5 mag with dark sky
4 images combined (dark
sky)
Data Processing
 Almost following the standard processing of
astronomical CCD photometry;
 Bias & dark corrections;
 Scattering light subtraction;
 Aperture photometry;
 Astrometry calibrations
 Flux calibrations with standard photometry stars;
 Pipelines have been developed with using the popular
astronomy software package, IRAF & Python.
Performance on the Moon V
Scattering light subtraction
 Dedicated pipelines were developed to subtract
the scattering light.
The scattering light imageCCD image
Subtracted image
Scientific results I
 Sky Survey in NUV
– Bright sources catalog (Meng+2016)
– 86 467 stars down to 16mag
Scientific results II
 Monitor of various variable stars hard to be done on ground
Identification of rapidly mass-transferring binary stars in a 6-
stars system!
AI Dra: Algol-type eclipsing binary
with P=1.1988 days.
Scientific results III
 The lowest upper limit on OH concentration in lunar
exosphere
Method Surface
concentration(cm-3)
HST spectroscopy <106(5σ)
Apollo12/14/15 CCGEs <107
Chandrayaan/CHACE <2 ×109
LUT background emission <4 ×104
Chandrayann-I M3 3μm OH absorption distrib
The End
Thanks

LUT on Chang'e-3

  • 1.
    Lunar Astronomy withthe LUT on Chang’e-3 lander National Astronomical Observatories, CAS/ Guangxi University J. Wang on behalf of LUT group Beijing 2018/12/07
  • 2.
    Contents  Lunar-based UltravioletTelescope  Performance on the Moon  Scientific results
  • 3.
    The dreams toobserve the Universe on the Moon Far UV camera with Appolo 16
  • 4.
     Lunar-based UltravioletTelescope (LUT, Cao+11)  A small, but automatic, telescope aboard CE-3 working in NUV. The FIRST automatic telescope landed on the extraterrestrial body in mankind history.  Scientific Objectives – Monitoring variable stars  Pulsating or binary stars, e.g., RR Lyr variables  Variable stars in clusters  Activities of solar-like stars – Survey the sky  Especially survey the low galactic latitude region;  Violent flare stars Lunar-based Ultraviolet Telescope I
  • 5.
     Milestones – July2004: Proposal Conception – Feb. 2009: Project Approval – Sep. 2009: Engineering Model – Dec. 2011: Flight Model – Dec. 02. 2013: Launch – Dec. 16. 2013: First Light – Jan. 2014 -- : Observations – The FIRST automatic telescope on the Moon for mankind. LUT First image RA. 16:45:00 Dec 50:26:00 (Draco) Lunar-based Ultraviolet Telescope II
  • 6.
  • 7.
    A supporting systemfor LUT scientific obs Exp vs S/N Ins. setup Finding chart & catalog Obs sequence head Obs sequence: Time slot Position of Gimbal Rotation step Target & comp coordinate
  • 8.
     Instrument Specifications Comp: Telescope+Pointing Reflector Item Value Diameter 150mm Focal Length 562.5mm Wavelength 245—340 nm Field of view 1.36  1.36 Square Degrees CCD camera E2V 47-20 UV enhanced Working time lunar day time Life time > one year Weight 13.6 kg Lunar-based Ultraviolet Telescope III
  • 9.
    Performance on theMoon I Sky Coverage: inside the red circle Pointing calibration Allow the telescope to point to any target & trace smoothly  Flux calibration – ~13.5 mag in lunar day time – ~15.5 mag with dark sky 4 images combined (dark sky)
  • 10.
    Data Processing  Almostfollowing the standard processing of astronomical CCD photometry;  Bias & dark corrections;  Scattering light subtraction;  Aperture photometry;  Astrometry calibrations  Flux calibrations with standard photometry stars;  Pipelines have been developed with using the popular astronomy software package, IRAF & Python. Performance on the Moon V
  • 11.
    Scattering light subtraction Dedicated pipelines were developed to subtract the scattering light. The scattering light imageCCD image Subtracted image
  • 12.
    Scientific results I Sky Survey in NUV – Bright sources catalog (Meng+2016) – 86 467 stars down to 16mag
  • 13.
    Scientific results II Monitor of various variable stars hard to be done on ground Identification of rapidly mass-transferring binary stars in a 6- stars system! AI Dra: Algol-type eclipsing binary with P=1.1988 days.
  • 14.
    Scientific results III The lowest upper limit on OH concentration in lunar exosphere Method Surface concentration(cm-3) HST spectroscopy <106(5σ) Apollo12/14/15 CCGEs <107 Chandrayaan/CHACE <2 ×109 LUT background emission <4 ×104 Chandrayann-I M3 3μm OH absorption distrib
  • 15.