Lunar Flashlight
Lunar Flashlight spaceprobe.jpeg
Lunar Flashlight nanosatellite
Mission typeLunar orbiter
OperatorNASA
COSPAR ID Edit this at Wikidata
Websitewww.jpl.nasa.gov/cubesat/missions/lunar_flashlight.php
Spacecraft properties
SpacecraftLunar Flashlight
Spacecraft typeCubeSat
Bus6U CubeSat[1]
ManufacturerJet Propulsion Laboratory (JPL)
Start of mission
Launch dateMarch 2023 (planned)[2]
RocketFalcon 9 Block 5
Launch siteKennedy LC-39A
ContractorSpaceX
Orbital parameters
Reference systemSelenocentric orbit
RegimePolar orbit
Periselene altitude20 km (12 mi) [3]
Aposelene altitude1000 to 5000 km
Inclination90°
Moon orbiter
Transponders
BandX-band
Capacity>10 kbps [4]
 

Lunar Flashlight is a planned low-cost CubeSat lunar orbiter mission to explore, locate, and estimate size and composition of water ice deposits on the Moon for future exploitation by robots or humans.[1][3][4][5][6][7]

The spacecraft, of the 6U CubeSat format, was developed by a team from the Jet Propulsion Laboratory (JPL), the Goddard Space Flight Center (GSFC), the Georgia Institute of Technology (GT), and NASA Marshall Space Flight Center.[5] It was selected in early 2015 by NASA's Advanced Exploration Systems (AES) for launch in 2022 as a secondary payload for the Artemis 1 mission, though it missed the integration window to be included on the mission.[8] Lunar Flashlight was remanifested to launch on Intuitive Machines' IM-1 mission in March 2023.[2]

History

NASA's Lunar Crater Observation and Sensing Satellite (LCROSS), the Lunar Reconnaissance Orbiter (LRO) and India's Chandrayaan-1 lunar orbiters and other missions discovered in 2009 both water (H2O) and hydroxyl (—OH) deposits at high latitudes on the lunar surface, indicating the presence of trace amounts of adsorbed or bound water are present.[3] These missions suggest that there might be enough ice water at polar regions to be used by future landed missions,[6][7] but the distribution is difficult to reconcile with thermal maps.[3]

Lunar prospecting missions are intended to pave the way toward incorporating use of space resources into mission architectures. NASA's planning for eventual Human mission to Mars depends on tapping the local natural resources to make oxygen and propellant for launching the return ship back to Earth, and a lunar precursor mission is a convenient location to test such in situ resource utilization (ISRU) technology.[9]

The mission concept was developed by a team from the Jet Propulsion Laboratory (JPL), the University of California, Los Angeles (UCLA), and NASA Marshall Space Flight Center and proposed to NASA's FY2014 Advanced Exploration Systems (AES) call.[3][5] The mission was selected for funding in early 2015.[6][10]

The initial concept considered using a solar sail.[6]
The initial concept considered using a solar sail.[6]

In its original conception, the Lunar Flashlight spacecraft would have been a 6U CubeSat format or bus propelled by an 80 m2 solar sail that would also have functioned as reflector to illuminate some selected permanently shadowed areas on the Moon,[6] while an onboard infrared spectrometer measured the reflected spectrum diagnostic of surface compositional mix among rock/dust, regolith, water ice, CO2, methane ice (CH4), and possibly ammonia ice (NH3).[3][4][6] The illuminated spot would have been about 400 m (1,300 ft) in diameter, reflected from an altitude of 20 km (12 mi).

Overview and objectives

The goal of Lunar Flashlight is to determine the presence or absence of exposed water ice and its physical state, and map its concentration at the 1-2 kilometer scale within the permanently shadowed regions of the lunar south pole.[5][11][12] The mission will be one of the first CubeSat to reach the Moon, and the first mission to use lasers to look for water ice.[1] Any polar volatile data collected by Lunar Flashlight could then ensure the most appropriate landing sites for a more expensive rover to perform in situ measurements and chemical analyses.[6] The spacecraft will maneuver to its lunar polar orbit and use its near infrared lasers to shine light into the shaded polar regions, while the on-board spectrometer measures surface reflection and composition.[1] Barbara Cohen from the NASA Marshall Space Flight Center is the principal investigator.[5]

Scientific payload

The proposed payload on this nanosatellite is an infrared spectrometer, consisting of a lens, dichroic beam splitters and multiple single-element detectors. It occupies 2 of the 6 modules of the 6U CubeSat bus.[3] The attitude control system (Blue Canyon Technologies' XACT-50), command and data handling, and power systems will occupy 1.5U; the Iris telecom system will occupy 0.5U.[4]

The Lunar Flashlight payload is derived from a few predecessor systems, including JPL's INSPIRE (Interplanetary Nano-Spacecraft Pathfinder In Relevant Environment), MARCO (Mars Cube One) and JPL's experience with spectrometers, including the Moon Mineralogy Mapper (M3).[1] The 6U CubeSat bus will use mostly commercial-off-the-shelf (COTS) components such as the lithium ion batteries, the CPU board, HaWK solar panels produced by MMA Design LLC, star tracker and 3-axis reaction wheels for attitude control.[3] The CPU is a "Rad-Tol Dependable Multiprocessor".[4] JPL will provide the Iris transponder that provides timing, navigation and telecommunication in the X band,[3] which is to be monitored with the NASA Deep Space Network.[4]

Launch

The spacecraft was initially planned to launch as a secondary payload on the maiden flight of the Space Launch System (SLS), Artemis 1, though it has since missed the integration window to be included on that flight.[8] It is now scheduled to launch in March 2023 as a secondary payload on the IM-1 mission.[2]

Proposed trajectory

The Lunar Flashlight spacecraft would have been ejected from the Space Launch System during its translunar flight, and will use a Sun sensor and solar panels to power the 3-axes reaction wheels. It also features a chemical monopropellant propulsion and orientation system built by the Georgia Tech Space System Design Laboratory.[13] The propulsion system occupies 3U of volume including 2 kg of monopropellant.[13]

The concept is that it will then begin a trajectory toward a multiple lunar, and possibly an Earth swingby transfer; it will be captured into a lunar polar orbit in one or two months after launch, depending on the selected trajectory.[3]

See also

The 10 CubeSats flying in the Artemis 1 mission
The 3 CubeSat missions not loaded onto Artemis 1

References

  1. ^ a b c d e "Lunar Flashlight Mission Information". JPL (NASA). April 2016. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  2. ^ a b c Eric Berger [@SciGuySpace] (16 September 2022). "Additionally, NASA has asked the company to land its IM-1 mission near the South Pole, instead of an equatorial region of the Moon. This has contributed to a slip in its launch on a Falcon 9 rocket to March 2023" (Tweet). Retrieved 16 September 2022 – via Twitter.
  3. ^ a b c d e f g h i j Cohen, Barbara A. (2013). Lunar Flashlight: Mapping lunar surface volatiles using a CubeSat (PDF). Annual Meeting of the Lunar Exploration Analysis Group (2013). NASA. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  4. ^ a b c d e f Hayne, P. O.; Cohen, B. A.; B. T., B. T. (21 March 2016). Lunar Flashlight: Illuminating the Moon's South Pole. 47th Lunar and Planetary Science Conference. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  5. ^ a b c d e "NASA TechPort: Lunar Flashlight Project". NASA TechPort. NASA. 2015. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  6. ^ a b c d e f g "Lunar Flashlight". Solar System Exploration Research Virtual Institute (SSERVI). NASA. 2015. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  7. ^ a b Wall, Mike (9 October 2014). "NASA Is Studying How to Mine the Moon for Water". SPACE.com. Retrieved 11 March 2021.
  8. ^ a b Ohana, Lavie (3 October 2021). "Four Artemis I CubeSats miss their ride". Space Scout. Retrieved 6 October 2021.
  9. ^ "NASA Looking to Mine Water on the Moon and Mars". Solar System Exploration Research Virtual Institute (SSERVI). NASA. 2015. Retrieved 11 March 2021. Public Domain This article incorporates text from this source, which is in the public domain.
  10. ^ Misra, Ria (2 February 2016). "NASA's New Mission to Mars Will Include a Giant Laser "Lunar Flashlight"". Gizmodo. Retrieved 11 March 2021.
  11. ^ "LUNAR FLASHLIGHT: MAPPING LUNAR SURFACE VOLATILES USING A CUBESAT" (PDF). Annual Meeting of the Lunar Exploration Analysis Group (2014). 2014. Retrieved 11 March 2021.
  12. ^ Cohen, Barbara (2016). "CubeSat for investigating ice on the Moon". SPIE Newsroom. SPIE.org. doi:10.1117/2.1201601.006241. ISSN 1818-2259. Retrieved 11 March 2021.
  13. ^ a b "Lunar Flashlight Propulsion System". Retrieved 23 April 2021.