Lunar Laser Ranging experiments

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Lunar Laser Ranging Experiment from the Apollo 11 mission Apollo 11 Lunar Laser Ranging Experiment.jpg
Lunar Laser Ranging Experiment from the Apollo 11 mission

Lunar Laser Ranging (LLR) is the practice of measuring the distance between the surfaces of the Earth and the Moon using laser ranging. The distance can be calculated from the round-trip time of laser light pulses travelling at the speed of light, which are reflected back to Earth by the Moon's surface or by one of several retroreflectors installed on the Moon. Three were placed by the United States' Apollo program (11, 14, and 15), two by the Soviet Lunokhod 1 and 2 missions, [1] and one by India's Chandrayaan-3 mission. [2] [3]

Contents

Although it is possible to reflect light or radio waves directly from the Moon's surface (a process known as EME), a much more precise range measurement can be made using retroreflectors, since because of their small size, the temporal spread in the reflected signal is much smaller. [4]

Laser ranging measurements can also be made with retroreflectors installed on Moon-orbiting satellites such as the LRO. [5] [6]

History

Apollo 15 LRRR ALSEP AS15-85-11468.jpg
Apollo 15 LRRR
Apollo 15 LRRR schematic Laser Ranging Retroreflector Apollo 15.svg
Apollo 15 LRRR schematic

The first successful lunar ranging tests were carried out in 1962 when Louis Smullin and Giorgio Fiocco from the Massachusetts Institute of Technology succeeded in observing laser pulses reflected from the Moon's surface using a laser with a 50J 0.5 millisecond pulse length. [7] Similar measurements were obtained later the same year by a Soviet team at the Crimean Astrophysical Observatory using a Q-switched ruby laser. [8]

Shortly thereafter, Princeton University graduate student James Faller proposed placing optical reflectors on the Moon to improve the accuracy of the measurements. [9] This was achieved following the installation of a retroreflector array on July 21, 1969 by the crew of Apollo 11. Two more retroreflector arrays were left by the Apollo 14 and Apollo 15 missions. Successful lunar laser range measurements to the retroreflectors were first reported on Aug. 1, 1969 by the 3.1 m telescope at Lick Observatory. [9] Observations from Air Force Cambridge Research Laboratories Lunar Ranging Observatory in Arizona, the Pic du Midi Observatory in France, the Tokyo Astronomical Observatory, and McDonald Observatory in Texas soon followed.

The uncrewed Soviet Lunokhod 1 and Lunokhod 2 rovers carried smaller arrays. Reflected signals were initially received from Lunokhod 1 by the Soviet Union up to 1974, but not by western observatories that did not have precise information about location. In 2010 NASA's Lunar Reconnaissance Orbiter located the Lunokhod 1 rover on images and in April 2010 a team from University of California ranged the array. [10] Lunokhod 2's array continues to return signals to Earth. [11] The Lunokhod arrays suffer from decreased performance in direct sunlight—a factor considered in reflector placement during the Apollo missions. [12]

The Apollo 15 array is three times the size of the arrays left by the two earlier Apollo missions. Its size made it the target of three-quarters of the sample measurements taken in the first 25 years of the experiment. Improvements in technology since then have resulted in greater use of the smaller arrays, by sites such as the Côte d'Azur Observatory in Nice, France; and the Apache Point Observatory Lunar Laser-ranging Operation (APOLLO) at the Apache Point Observatory in New Mexico.

In the 2010s several new retroreflectors were planned. The MoonLIGHT reflector, which was to be placed by the private MX-1E lander, was designed to increase measurement accuracy up to 100 times over existing systems. [13] [14] [15] MX-1E was set to launch in July 2020, [16] however, as of February 2020, the launch of the MX-1E has been canceled. [17] India's Chandrayaan-3 lunar lander successfully placed a sixth reflector on the Moon in August 2023. [3] MoonLIGHT will be launched in early 2024 with a Commercial Lunar Payload Services (CLPS) mission. [18]

Principle

Annotated image of the near side of the Moon showing the location of retroreflectors left on the surface by Apollo and Lunokhod missions Lunar retroreflector locations.jpg
Annotated image of the near side of the Moon showing the location of retroreflectors left on the surface by Apollo and Lunokhod missions

The distance to the Moon is calculated approximately using the equation: distance = (speed of light × duration of delay due to reflection) / 2. Since the speed of light is a defined constant, conversion between distance and time of flight can be made without ambiguity.

To compute the lunar distance precisely, many factors must be considered in addition to the round-trip time of about 2.5 seconds. These factors include the location of the Moon in the sky, the relative motion of Earth and the Moon, Earth's rotation, lunar libration, polar motion, weather, speed of light in various parts of air, propagation delay through Earth's atmosphere, the location of the observing station and its motion due to crustal motion and tides, and relativistic effects. [20] [21] The distance continually changes for a number of reasons, but averages 385,000.6 km (239,228.3 mi) between the center of the Earth and the center of the Moon. [22] The orbits of the Moon and planets are integrated numerically along with the orientation of the Moon called physical libration. [23]

At the Moon's surface, the beam is about 6.5 kilometers (4.0 mi) wide [24] [lower-roman 1] and scientists liken the task of aiming the beam to using a rifle to hit a moving dime 3 kilometers (1.9 mi) away. The reflected light is too weak to see with the human eye. Out of a pulse of 3×1017 photons [25] aimed at the reflector, only about 1–5 are received back on Earth, even under good conditions. [26] They can be identified as originating from the laser because the laser is highly monochromatic.

As of 2009, the distance to the Moon can be measured with millimeter precision. [27] In a relative sense, this is one of the most precise distance measurements ever made, and is equivalent in accuracy to determining the distance between Los Angeles and New York to within the width of a human hair.

List of retroreflectors

List of observatories

The table below presents a list of active and inactive Lunar Laser Ranging stations on Earth. [22] [28]

Lunar Laser Ranging stations
ObservatoryProjectOperating timespanTelescopeLaserRange accuracyRef.
McDonald Observatory, Texas, USMLRS1969–1985

1985–2013

2.7 m694 nm, 7 J

532 nm, 200 ps, 150 mJ

 [29]

[22]

Crimean Astrophysical Observatory (CrAO), USSR1974, 1982–1984694 nm3.0–0.6 m [30]
Côte d'Azur Observatory (OCA), Grasse, FranceMeO1984–1986

1986–2010

2010–present (2021)

694 nm

532 nm, 70 ps, 75 mJ

532/1064 nm

 [22] [31]
Haleakala Observatory, Hawaii, USLURE1984–1990532 nm, 200 ps, 140 mJ2.0 cm [22] [32]
Matera Laser Ranging Observatory (MLRO), Italy2003–present (2021)532 nm
Apache Point Observatory, New Mexico, US APOLLO 2006–2021

2021–present (2023)

532 nm, 100 ps, 115 mJ1.1 mm [22]

[33]

Geodetic Observatory Wettzell, GermanyWLRS2018–present (2021)1064 nm, 10 ps, 75 mJ [34]
Yunnan Astronomical Observatory, Kunming, China20181.2 m532 nm, 10 ns, 3 Jmeter level [35]

Data analysis

The Lunar Laser Ranging data is collected in order to extract numerical values for a number of parameters. Analyzing the range data involves dynamics, terrestrial geophysics, and lunar geophysics. The modeling problem involves two aspects: an accurate computation of the lunar orbit and lunar orientation, and an accurate model for the time of flight from an observing station to a retroreflector and back to the station. Modern Lunar Laser Ranging data can be fit with a 1 cm weighted rms residual.

The range model includes [36] [37]

For the terrestrial model, the IERS Conventions (2010) is a source of detailed information. [38]

Results

Lunar laser ranging measurement data is available from the Paris Observatory Lunar Analysis Center, [39] the International Laser Ranging Service archives, [40] [41] and the active stations. Some of the findings of this long-term experiment are: [22]

Properties of the Moon

Gravitational physics

See also

Related Research Articles

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<span class="mw-page-title-main">Corner reflector</span> Retroreflector with three orthogonal, intersecting flat surfaces

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References

  1. ↑ During the round-trip time, an Earth observer will have moved by around 1 km (depending on their latitude). This has been presented, incorrectly, as a 'disproof' of the ranging experiment, the claim being that the beam to such a small reflector cannot hit such a moving target. However the size of the beam is far larger than any movement, especially for the returned beam.
  1. ↑ Chapront, J.; Chapront-Touzé, M.; Francou, G. (1999). "Determination of the lunar orbital and rotational parameters and of the ecliptic reference system orientation from LLR measurements and IERS data". Astronomy and Astrophysics . 343: 624–633. Bibcode:1999A&A...343..624C.
  2. ↑ "Chandrayaan-3". ISRO. Retrieved 15 August 2023.
  3. 1 2 Dhillon, Amrit (23 August 2023). "India lands spacecraft near south pole of moon in historic first". The Guardian . Retrieved 23 August 2023.
  4. ↑ Müller, Jürgen; Murphy, Thomas W.; Schreiber, Ulrich; Shelus, Peter J.; Torre, Jean-Marie; Williams, James G.; Boggs, Dale H.; Bouquillon, Sebastien; Bourgoin, Adrien; Hofmann, Franz (2019). "Lunar Laser Ranging: a tool for general relativity, lunar geophysics and Earth science". Journal of Geodesy. 93 (11): 2195–2210. Bibcode:2019JGeod..93.2195M. doi:10.1007/s00190-019-01296-0. ISSN   1432-1394. S2CID   202641440.
  5. ↑ Mazarico, Erwan; Sun, Xiaoli; Torre, Jean-Marie; Courde, Clément; Chabé, Julien; Aimar, Mourad; Mariey, Hervé; Maurice, Nicolas; Barker, Michael K.; Mao, Dandan; Cremons, Daniel R.; Bouquillon, Sébastien; Carlucci, Teddy; Viswanathan, Vishnu; Lemoine, Frank; Bourgoin, Adrien; Exertier, Pierre; Neumann, Gregory; Zuber, Maria; Smith, David (6 August 2020). "First two-way laser ranging to a lunar orbiter: infrared observations from the Grasse station to LRO's retro-reflector array". Earth, Planets and Space. 72 (1): 113. Bibcode:2020EP&S...72..113M. doi: 10.1186/s40623-020-01243-w . hdl: 11603/19523 . ISSN   1880-5981.
  6. ↑ Kornei, Katherine (15 August 2020). "How Do You Solve a Moon Mystery? Fire a Laser at It". The New York Times. ISSN   0362-4331 . Retrieved 1 June 2021.
  7. ↑ Smullin, Louis D.; Fiocco, Giorgio (1962). "Optical Echoes from the Moon". Nature . 194 (4835): 1267. Bibcode:1962Natur.194.1267S. doi: 10.1038/1941267a0 . S2CID   4145783.
  8. ↑ Bender, P. L.; et al. (1973). "The Lunar Laser Ranging Experiment: Accurate ranges have given a large improvement in the lunar orbit and new selenophysical information" (PDF). Science . 182 (4109): 229–238. Bibcode:1973Sci...182..229B. doi:10.1126/science.182.4109.229. PMID   17749298. S2CID   32027563.
  9. 1 2 Newman, Michael E. (26 September 2017). "To the Moon and Back … in 2.5 Seconds". NIST. Retrieved 27 January 2021.
  10. ↑ McDonald, K. (26 April 2010). "UC San Diego Physicists Locate Long Lost Soviet Reflector on Moon". University of California, San Diego. Archived from the original on 30 April 2010. Retrieved 27 April 2010.
  11. 1 2 3 Williams, James G.; Dickey, Jean O. (2002). Lunar Geophysics, Geodesy, and Dynamics (PDF). 13th International Workshop on Laser Ranging. 7–11 October 2002. Washington, D. C.
  12. ↑ "It's Not Just The Astronauts That Are Getting Older". Universe Today . 10 March 2010. Retrieved 24 August 2012.
  13. ↑ Currie, Douglas; Dell'Agnello, Simone; Delle Monache, Giovanni (April–May 2011). "A Lunar Laser Ranging Retroreflector Array for the 21st Century". Acta Astronautica. 68 (7–8): 667–680. Bibcode:2011AcAau..68..667C. doi:10.1016/j.actaastro.2010.09.001.
  14. ↑ Tune, Lee (10 June 2015). "UMD, Italy & MoonEx Join to Put New Laser-Reflecting Arrays on Moon". UMD Right Now. University of Maryland. Archived from the original on 22 March 2018. Retrieved 21 March 2018.
  15. ↑ Boyle, Alan (12 July 2017). "Moon Express unveils its roadmap for giant leaps to the lunar surface ... and back again". GeekWire. Retrieved 15 March 2018.
  16. ↑ Moon Express Lunar Scout (MX-1E), RocketLaunch.Live, archived from the original on 27 July 2019, retrieved 27 July 2019
  17. ↑ "MX-1E 1, 2, 3" . Retrieved 24 May 2020.
  18. ↑ "NASA Payloads for (CLPS PRISM) CP-11".
  19. ↑ "Was Galileo Wrong?". NASA. 6 May 2004. Archived from the original on 30 April 2022.
  20. ↑ Seeber, Günter (2003). Satellite Geodesy (2nd ed.). de Gruyter. p.  439. ISBN   978-3-11-017549-3. OCLC   52258226.
  21. ↑ Williams, James G.; Boggs, Dale H. (2020). "The JPL Lunar Laser range model 2020". ssd.jpl.nasa.gov. Retrieved 24 May 2021.
  22. 1 2 3 4 5 6 7 Murphy, T. W. (2013). "Lunar laser ranging: the millimeter challenge" (PDF). Reports on Progress in Physics . 76 (7): 2. arXiv: 1309.6294 . Bibcode:2013RPPh...76g6901M. doi:10.1088/0034-4885/76/7/076901. PMID   23764926. S2CID   15744316.
  23. 1 2 Park, Ryan S.; Folkner, William M.; Williams, James G.; Boggs, Dale H. (2021). "The JPL Planetary and Lunar Ephemerides DE440 and DE441". The Astronomical Journal. 161 (3): 105. Bibcode:2021AJ....161..105P. doi: 10.3847/1538-3881/abd414 . ISSN   1538-3881. S2CID   233943954.
  24. 1 2 Espenek, F. (August 1994). "NASA – Accuracy of Eclipse Predictions". NASA/GSFC. Retrieved 4 May 2008.
  25. ↑ "The Basics of Lunar Ranging" . Retrieved 21 July 2023.
  26. ↑ Merkowitz, Stephen M. (2 November 2010). "Tests of Gravity Using Lunar Laser Ranging". Living Reviews in Relativity. 13 (1): 7. Bibcode:2010LRR....13....7M. doi:10.12942/lrr-2010-7. ISSN   1433-8351. PMC   5253913 . PMID   28163616.
  27. 1 2 Battat, J. B. R.; Murphy, T. W.; Adelberger, E. G.; et al. (January 2009). "The Apache Point Observatory Lunar Laser-ranging Operation (APOLLO): Two Years of Millimeter-Precision Measurements of the Earth-Moon Range1". Publications of the Astronomical Society of the Pacific. 121 (875): 29–40. Bibcode:2009PASP..121...29B. doi: 10.1086/596748 . JSTOR   10.1086/596748.
  28. ↑ Biskupek, Liliane; Müller, Jürgen; Torre, Jean-Marie (3 February 2021). "Benefit of New High-Precision LLR Data for the Determination of Relativistic Parameters". Universe. 7 (2): 34. arXiv: 2012.12032 . Bibcode:2021Univ....7...34B. doi: 10.3390/universe7020034 .
  29. ↑ Bender, P. L.; Currie, D. G.; Dickey, R. H.; Eckhardt, D. H.; Faller, J. E.; Kaula, W. M.; Mulholland, J. D.; Plotkin, H. H.; Poultney, S. K.; et al. (1973). "The Lunar Laser Ranging Experiment". Science. 182 (4109): 229–238. Bibcode:1973Sci...182..229B. doi:10.1126/science.182.4109.229. ISSN   0036-8075. PMID   17749298. S2CID   32027563.
  30. ↑ Yagudina (2018). "Processing and analysis of lunar laser ranging observations in Crimea in 1974-1984". Institute of Applied Astronomy of the Russian Academy of Sciences. Retrieved 1 June 2021.
  31. ↑ Chabé, Julien; Courde, Clément; Torre, Jean-Marie; Bouquillon, Sébastien; Bourgoin, Adrien; Aimar, Mourad; Albanèse, Dominique; Chauvineau, Bertrand; Mariey, Hervé; Martinot-Lagarde, Grégoire; Maurice, Nicolas (2020). "Recent Progress in Lunar Laser Ranging at Grasse Laser Ranging Station". Earth and Space Science. 7 (3): e2019EA000785. Bibcode:2020E&SS....700785C. doi: 10.1029/2019EA000785 . ISSN   2333-5084. S2CID   212785296.
  32. ↑ "Lure Observatory". Institute for Astronomy, University of Hawaii. 29 January 2002. Retrieved 3 June 2021.
  33. ↑ "APOL - Apache Point Observatory".
  34. ↑ Eckl, Johann J.; Schreiber, K. Ulrich; Schüler, Torben (30 April 2019). "Lunar laser ranging utilizing a highly efficient solid-state detector in the near-IR". In Domokos, Peter; James, Ralph B; Prochazka, Ivan; Sobolewski, Roman; Gali, Adam (eds.). Quantum Optics and Photon Counting 2019. Vol. 11027. International Society for Optics and Photonics. p. 1102708. Bibcode:2019SPIE11027E..08E. doi:10.1117/12.2521133. ISBN   9781510627208. S2CID   155720383.
  35. ↑ Li Yuqiang, 李语强; Fu Honglin, 伏红林; Li Rongwang, 李荣旺; Tang Rufeng, 汤儒峰; Li Zhulian, 李祝莲; Zhai Dongsheng, 翟东升; Zhang Haitao, 张海涛; Pi Xiaoyu, 皮晓宇; Ye Xianji, 叶贤基; Xiong Yaoheng, 熊耀恒 (27 January 2019). "Research and Experiment of Lunar Laser Ranging in Yunnan Observatories". Chinese Journal of Lasers. 46 (1): 0104004. doi:10.3788/CJL201946.0104004. S2CID   239211201.
  36. 1 2 Pavlov, Dmitry A.; Williams, James G.; Suvorkin, Vladimir V. (2016). "Determining parameters of Moon's orbital and rotational motion from LLR observations using GRAIL and IERS-recommended models". Celestial Mechanics and Dynamical Astronomy. 126 (1): 61–88. arXiv: 1606.08376 . Bibcode:2016CeMDA.126...61P. doi:10.1007/s10569-016-9712-1. ISSN   0923-2958. S2CID   119116627.
  37. ↑ Williams, James G.; Boggs, Dale H. (2020). "The JPL Lunar Laser range model 2020". ssd.jpl.nasa.gov. Retrieved 1 June 2021.
  38. ↑ "IERS - IERS Technical Notes - IERS Conventions (2010)". www.iers.org. Retrieved 1 June 2021.
  39. ↑ "Lunar Laser Ranging Observations from 1969 to May 2013". SYRTE Paris Observatory. Retrieved 3 June 2014.
  40. ↑ "International Laser Ranging Service".
  41. ↑ "International Laser Ranging Service".
  42. 1 2 Williams, James G.; Boggs, Dale H. (2016). "Secular tidal changes in lunar orbit and Earth rotation". Celestial Mechanics and Dynamical Astronomy. 126 (1): 89–129. Bibcode:2016CeMDA.126...89W. doi:10.1007/s10569-016-9702-3. ISSN   0923-2958. S2CID   124256137.
  43. ↑ Bills, B. G.; Ray, R. D. (1999). "Lunar Orbital Evolution: A Synthesis of Recent Results". Geophysical Research Letters . 26 (19): 3045–3048. Bibcode:1999GeoRL..26.3045B. doi: 10.1029/1999GL008348 .
  44. ↑ Williams, James G.; Boggs, Dale H.; Yoder, Charles F.; Ratcliff, J. Todd; Dickey, Jean O. (2001). "Lunar rotational dissipation in solid body and molten core". Journal of Geophysical Research: Planets. 106 (E11): 27933–27968. Bibcode:2001JGR...10627933W. doi: 10.1029/2000JE001396 .
  45. ↑ Rambaux, N.; Williams, J. G. (2011). "The Moon's physical librations and determination of their free modes" (PDF). Celestial Mechanics and Dynamical Astronomy. 109 (1): 85–100. Bibcode:2011CeMDA.109...85R. doi:10.1007/s10569-010-9314-2. S2CID   45209988.
  46. 1 2 3 Viswanathan, V.; Rambaux, N.; Fienga, A.; Laskar, J.; Gastineau, M. (9 July 2019). "Observational Constraint on the Radius and Oblateness of the Lunar Core‐Mantle Boundary". Geophysical Research Letters . 46 (13): 7295–7303. arXiv: 1903.07205 . Bibcode:2019GeoRL..46.7295V. doi:10.1029/2019GL082677. S2CID   119508748.
  47. ↑ Wagner, R. V.; Nelson, D. M.; Plescia, J. B.; Robinson, M. S.; Speyerer, E. J.; Mazarico, E. (2017). "Coordinates of anthropogenic features on the Moon". Icarus. 283: 92–103. Bibcode:2017Icar..283...92W. doi: 10.1016/j.icarus.2016.05.011 . ISSN   0019-1035.
  48. 1 2 Williams, J. G.; Newhall, X. X.; Dickey, J. O. (1996). "Relativity parameters determined from lunar laser ranging". Physical Review D . 53 (12): 6730–6739. Bibcode:1996PhRvD..53.6730W. doi:10.1103/PhysRevD.53.6730. PMID   10019959.
  49. ↑ Kopeikin, S.; Xie, Y. (2010). "Celestial reference frames and the gauge freedom in the post-Newtonian mechanics of the Earth–Moon system". Celestial Mechanics and Dynamical Astronomy . 108 (3): 245–263. Bibcode:2010CeMDA.108..245K. doi:10.1007/s10569-010-9303-5. S2CID   122789819.
  50. ↑ Adelberger, E. G.; Heckel, B. R.; Smith, G.; Su, Y.; Swanson, H. E. (1990). "Eötvös experiments, lunar ranging and the strong equivalence principle". Nature . 347 (6290): 261–263. Bibcode:1990Natur.347..261A. doi:10.1038/347261a0. S2CID   4286881.
  51. ↑ Viswanathan, V; Fienga, A; Minazzoli, O; Bernus, L; Laskar, J; Gastineau, M (May 2018). "The new lunar ephemeris INPOP17a and its application to fundamental physics". Monthly Notices of the Royal Astronomical Society. 476 (2): 1877–1888. arXiv: 1710.09167 . Bibcode:2018MNRAS.476.1877V. doi:10.1093/mnras/sty096.
  52. ↑ Müller, J.; Biskupek, L. (2007). "Variations of the gravitational constant from lunar laser ranging data". Classical and Quantum Gravity . 24 (17): 4533. doi:10.1088/0264-9381/24/17/017. S2CID   120195732.
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