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Lunar Laser Ranging experiments

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Lunar Laser Ranging Experiment from the Apollo 11 mission

Lunar Laser Ranging(LLR) is the practice of measuringthe distancebetween the surfaces of theEarthand theMoonusinglaser ranging.The distance can be calculated from theround-trip timeoflaserlight pulses travelling at thespeed of light,which are reflected back to Earth by the Moon's surface or byone of severalretroreflectorsinstalled on the Moon. Three were placed by the United States'Apollo program(11,14,and15), two by the SovietLunokhod 1 and 2 missions,[1]and one by India'sChandrayaan-3mission.[2][3]

Although it is possible to reflect light or radio waves directly from the Moon's surface (a process known asEME), 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]and because the return will be more evenly reflected with less diffusion.

Laser ranging measurements can also be made with retroreflectors installed onMoon-orbiting satellitessuch as theLRO.[5][6]

History[edit]

Apollo 15 LRRR
Apollo 15 LRRR schematic

The first successful lunar ranging tests were carried out in 1962 whenLouis SmullinandGiorgio Fioccofrom theMassachusetts Institute of Technologysucceeded 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 theCrimean Astrophysical Observatoryusing aQ-switchedruby laser.[8]

Shortly thereafter,Princeton Universitygraduate studentJames Fallerproposed placing optical reflectors on the Moon to improve the accuracy of the measurements.[9]This was achieved following the installation of aretroreflectorarray on July 21, 1969 by the crew ofApollo 11.Two more retroreflector arrays were left by theApollo 14andApollo 15missions. Successful lunar laser range measurements to theretroreflectorswere first reported on Aug. 1, 1969 by the 3.1 m telescope atLick Observatory.[9]Observations fromAir Force Cambridge Research LaboratoriesLunar Ranging Observatory in Arizona, thePic du Midi Observatoryin France, the TokyoAstronomical Observatory,andMcDonald Observatoryin Texas soon followed.

The uncrewed SovietLunokhod 1andLunokhod 2rovers carried smaller arrays. Reflected signals were initially received fromLunokhod 1by the Soviet Union up to 1974, but not by western observatories that did not have precise information about location. In 2010NASA'sLunar Reconnaissance Orbiterlocated the Lunokhod 1 rover on images and in April 2010 a team from University of California ranged the array.[10]Lunokhod 2'sarray 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 theCôte d'Azur ObservatoryinNice,France; and theApache Point Observatory Lunar Laser-ranging Operation(APOLLO) at theApache Point ObservatoryinNew Mexico.

In the 2010s severalnew retroreflectorswere planned. TheMoonLIGHTreflector, which was to be placed by the privateMX-1Elander, 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'sChandrayaan-3lunar lander successfully placed a sixth reflector on the Moon in August 2023.[3]MoonLIGHT will be launched in early 2024 with aCommercial Lunar Payload Services(CLPS) mission.[18]

Principle[edit]

See also:Apache Point Observatory Lunar Laser-ranging Operation § Principle of operation
Annotated image of the near side of the Moon showing the location of retroreflectors left on the surface by Apollo and Lunokhod missions[19]

The distance to the Moon is calculatedapproximatelyusing the equation: distance= (speed of light×duration of delay due to reflection) / 2.Since thespeed of lightis 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 throughEarth's atmosphere,the location of the observing station and its motion due tocrustal motionandtides,andrelativistic 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 physicallibration.[23]

At the Moon's surface, the beam is about 6.5 kilometers (4.0 mi) wide[24][i]and scientists liken the task of aiming the beam to using a rifle to hit a movingdime3 kilometers (1.9 mi) away. The reflected light is too weak to see with the human eye. Out of a pulse of 3×1017photons[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 highlymonochromatic.

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[edit]

Main article:List of retroreflectors on the Moon

List of observatories[edit]

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

Lunar Laser Ranging stations
Observatory Project Operating timespan Telescope Laser Range accuracy Ref.
McDonald Observatory,Texas, US MLRS 1969–1985

1985–2013

2.7 m 694 nm, 7 J

532 nm, 200 ps, 150 mJ

[29]

[22]

Crimean Astrophysical Observatory(CrAO), USSR 1974, 1982–1984 694 nm 3.0–0.6 m [30]
Côte d'Azur Observatory(OCA), Grasse, France MeO 1984–1986

1986–2010

2010–present (2021)

694 nm

532 nm, 70 ps, 75 mJ

532/1064 nm

[22][31]
Haleakala Observatory,Hawaii, US LURE 1984–1990 532 nm, 200 ps, 140 mJ 2.0 cm [22][32]
Matera Laser Ranging Observatory (MLRO), Italy 2003–present (2021) 532 nm
Apache Point Observatory,New Mexico, US APOLLO 2006–2021

2021–present (2023)

532 nm, 100 ps, 115 mJ 1.1 mm [22]

[33]

Geodetic Observatory Wettzell,Germany WLRS 2018–present (2021) 1064 nm, 10 ps, 75 mJ [34]
Yunnan Astronomical Observatory,Kunming, China 2018 1.2 m 532 nm, 10 ns, 3 J meter level [35]

Data analysis[edit]

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 center of Earth to center of Moon distance is computed by a program that numerically integrates the lunar and planetary orbits accounting for the gravitational attraction of the Sun, planets, and a selection of asteroids.[36][23]
  • The same program integrates the 3-axis orientation of the Moon called physicalLibration.

The range model includes[36][37]

  • The position of the ranging station accounting for motion due toplate tectonics,Earth rotation,precession,nutation,andpolar motion.
  • Tides in the solid Earth and seasonal motion of the solid Earth with respect to its center of mass.
  • Relativistic transformation of time and space coordinates from a frame moving with the station to a frame fixed with respect to the solar system center of mass. Lorentz contraction of the Earth is part of this transformation.
  • Delay in the Earth's atmosphere.
  • Relativistic delay due to the gravity fields of the Sun, Earth, and Moon.
  • The position of the retroreflector accounting for orientation of the Moon and solid-body tides.
  • Lorentz contraction of the Moon.
  • Thermal expansion and contraction of the retroreflector mounts.

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

Results[edit]

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 thislong-term experimentare:[22]

Properties of the Moon[edit]

  • The distance to the Moon can be measured with millimeter precision.[27]
  • The Moon is spiraling away from Earth at a rate of3.8 cm/year.[24][42]This rate has been described as anomalously high.[43]
  • The fluid core of the Moon was detected from the effects of core/mantle boundary dissipation.[44]
  • The Moon has free physicallibrationsthat require one or more stimulating mechanisms.[45]
  • Tidal dissipation in the Moon depends on tidal frequency.[42]
  • The Moon probably has a liquid core of about 20% of the Moon's radius.[11]The radius of the lunar core-mantle boundary is determined as381±12 km.[46]
  • The polarflatteningof the lunar core-mantle boundary is determined as(2.2±0.6)×10−4.[46]
  • The free corenutationof the Moon is determined as367±100 yr.[46]
  • Accurate locations for retroreflectors serve as reference points visible to orbiting spacecraft.[47]

Gravitational physics[edit]

Gallery[edit]

See also[edit]

References[edit]

  1. ^During the round-trip time, an Earth observer will have moved by around1 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.
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External links[edit]

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