Lunar Atmosphere and Dust Environment Explorer
Artist's depiction of LADEE in lunar orbit
|Mission type||Lunar atmospheric research|
|Mission duration||Primary mission: 100 days
Extended mission: 28 days
|Manufacturer||Ames Research Center|
|Launch mass||383 kg (844 lb)|
|Dry mass||248 kg (547 lb)|
|Start of mission|
|Launch date||September 7, 2013, 03:27UTC|
|Launch site||MARS LP-0B|
|Contractor||Orbital Sciences Corporation|
|Periselene||20 km (12 mi)|
|Aposelene||60 km (37 mi)|
|Epoch||Planned (science phase)|
|Orbital insertion||October 6, 2013, 10:57 UTC|
The Lunar Atmosphere and Dust Environment Explorer (LADEE, pronounced //) is a NASA lunar exploration mission led by Ames Research Center in collaboration with Goddard Space Flight Center. It was launched on a Minotaur V from the Mid-Atlantic Regional Spaceport on September 7, 2013, at 03:27 UTC. During its nominal 100-day scientific mission, LADEE will orbit around the Moon's equator, and use instruments aboard the spacecraft to study the lunar exosphere and dust in the Moon's vicinity. Instruments include a dust detector, a neutral mass spectrometer, and an ultraviolet-visible spectrometer, as well as a technology demonstration consisting of a laser communications terminal. (see Free-space optical communication "lasercom")
- 1 History
- 2 Mission objectives
- 3 Spaceflight operations
- 4 Spacecraft
- 5 Preliminary results
- 6 Team
- 7 Image gallery
- 8 References
- 9 External links
LADEE was announced during the presentation of NASA's FY09 budget in February 2008. It was initially planned to be launched with the Gravity Recovery and Interior Laboratory (GRAIL) satellites. The full-scale thermal vacuum chamber testing was performed at NASA's Ames Research Center in April 2013. Previous mechanical tests—including acoustic, vibration and shock—were completed prior to the thermal-vacuum testing. During August 2013, LADEE underwent final balancing, fuelling and mounting on the launcher, and all pre-launch activities were complete by August 31, ready for the launch window which opened on September 6.
NASA Ames is responsible for the day-to-day functions of LADEE while the Goddard Space Flight Center operates the sensor suite and technology demonstration payloads as well as managing launch operations. The LADEE mission totals approximately $280 million, which includes spacecraft development and science instruments, launch services, mission operations, science processing and relay support.
There is some evidence that the Moon may have a tenuous atmosphere of moving particles constantly leaping up from and falling back to the Moon's surface, giving rise to a "dust atmosphere" that looks static but is composed of dust particles in constant motion. According to models proposed starting from 1956, on the daylit side of the Moon, solar ultraviolet and X-ray radiation is energetic enough to knock electrons out of atoms and molecules in the lunar soil. Positive charges build up until the tiniest particles of lunar dust (measuring 1 micrometre and smaller) are repelled from the surface and lofted anywhere from metres to kilometres high, with the smallest particles reaching the highest altitudes. Eventually they fall back toward the surface where the process is repeated. On the night side, the dust is negatively charged by electrons in the solar wind. Indeed, the "fountain model" suggests that the night side would charge up to higher voltages than the day side, possibly launching dust particles to higher velocities and altitudes. This effect could be further enhanced during the portion of the Moon's orbit where it passes through Earth's magnetotail; see Magnetic field of the Moon for more detail. On the terminator there could be significant horizontal electric fields forming between the day and night areas, resulting in horizontal dust transport.
Also, the Moon has been shown to have a "sodium tail" too faint to be detected by the human eye. It is hundreds of thousands of miles long, and was discovered in 1998 as a result of Boston University scientists observing the Leonid meteor storm. The Moon is constantly releasing atomic sodium gas from its surface, and solar radiation pressure accelerates the sodium atoms in the anti-sunward direction, forming an elongated tail which points away from the Sun. It is to be determined if ionized sodium gas atoms or charged dust are the cause of the reported Moon glows.
China's Chang'e 3 spacecraft, which was launched on December 1, 2013, and entered lunar orbit on December 6, is expected to contaminate the tenuous lunar exosphere with both propellant from engine firings and lunar dust from the vehicle's landing. While concern was expressed that this could disrupt LADEE's mission, such as its baseline readings of the Moon's exosphere, it may instead provide additional science value since both the quantity and composition of the spacecraft's propulsion system exhaust is known. LADEE may be able to track the distribution and eventual dissipation of the exhaust and dust in the Moon's exosphere. It may also be able to observe the migration of water, one of the exhaust's components, giving insight on how it is transported and becomes trapped around the lunar poles.
LADEE mission will address three major science goals:
- Determine the global density, composition, and time variability of the tenuous lunar exosphere before it is perturbed by further human activity.
- Determine if the Apollo astronaut sightings of diffuse emission at tens of kilometers above the surface were sodium glow or dust.
- Document the dust impactor environment (size-frequency) to help guide design engineering for the outpost and also future robotic missions.
LADEE was launched on September 7, 2013, at 03:27 UTC (September 6, 11:27 p.m. EDT) out of the Wallops Flight Facility at the Mid-Atlantic Regional Spaceport on a Minotaur V carrier rocket. This was the first lunar mission to be launched from that facility. The launch had the potential for visibility along much of the U.S. eastern seaboard, from Maine to South Carolina; clear weather allowed numerous observers from New York City to Virginia to observe the ascent, first stage cutoff and second stage ignition.
As the Minotaur V is a solid-propellant rocket, spacecraft attitude control on this mission operated a bit differently than on a typical liquid-fueled rocket with more continuous closed-loop feedback. The first three Minotaur stages "fly a pre-programmed attitude profile" to gain velocity and deliver the vehicle to its preliminary trajectory, while the fourth stage is used to modify the flight profile and deliver the LADEE spacecraft into perigee for the spin-stabilized fifth stage to then put the spacecraft into a highly-elliptical orbit around Earth—the first of three—to begin a month-long Lunar transit.
LADEE took an unusual approach in its transit of the Moon. Launched into a highly elliptical Earth orbit, the spacecraft made three increasingly-larger laps around Earth before getting close enough to enter into Lunar orbit. The transit required approximately one month.
After separating from the Minotaur, high electrical currents were detected in the satellite's reaction wheels causing them to be shut down. There was no indication of a fault, and after the protection limits were adjusted orientation with reaction wheels was resumed the following day.
The LADEE spacecraft made three "phasing orbits" of Earth before it accomplished a Lunar orbit insertion (LOI), which occurred at perigee of the third orbit using a three-minute engine burn. The target orbit for the third Earth orbit had a perigee of 200 kilometers (120 mi), an apogee of 278,000 km (173,000 mi) and an inclination of 37.65 degrees. The planned argument of perigee is 155 degrees, while its characteristic energy, C3 is -2.75 km2/s2. The novel trajectory using orbital phasing loops was done for four main reasons:
- The Minotaur V launch vehicle had insufficient delta-v to put the 383 kg (844 lb) LADEE directly into a trans-lunar injection.
- To handle potential off-nominal launch dispersions from the Minotaur V—which is a stack of five solid rocket stages, and is not considered to be a particularly precise rocket—in a propellant-efficient manner while leaving the orbit profile flexible to large dispersions in the initial injection orbit.
- To widen the launch window to five days. In the event, LADEE did not need this as the launch occurred at the beginning of the window on the first day.
- To increase mission robustness in the face of any anomalous or missed orbital maneuvers with the spacecraft.
Lunar orbit and systems checkout
LADEE entered lunar orbit on October 6, 2013, when LADEE was put into an elliptical capture orbit of 24 hours duration. LADEE was further lowered into a four-hour orbit on October 9, 2013, One further burn occurred on October 12 lowering LADEE into a circular orbit around the Moon with an altitude of approximately 250 kilometers (160 mi) for its commissioning phase, which will last about 30 days. LADEE's systems and instruments are planned to be checked out when the orbit is lowered to 75 km (47 mi) altitude.
Lunar Laser Communication Demonstration
LADEE's Lunar Laser Communication Demonstration (LLCD) pulsed laser system conducted a successful test on October 18, 2013, transmitting data between the spacecraft and its ground station on Earth at a distance of 385,000 kilometres (239,000 mi). This test set a downlink record of 622 megabits per second (Mbps) from spacecraft to ground, and an "error-free data upload rate of 20 Mbps" from ground station to spacecraft.
The LLCD is NASA's first attempt at two-way space communication using an optical laser instead of radio waves, and is expected to lead to operational laser systems on future NASA satellites. The next iteration of the concept will be the Laser Communications Relay Demonstration scheduled for 2017.
For the science operations, LADEE will be maneuvered into an orbit with a periselene of 20 km (12 mi) and an aposelene of 60 km (37 mi). The science phase of LADEE’s primary mission was 100 days, and later, it was given a 28 day extension. The extension provides an opportunity for the satellite to gather an additional full lunar cycle worth of very low-altitude data to help scientists unravel the nature of the Moon's tenuous exosphere.
LADEE is the first spacecraft ever designed, integrated, built, and tested by NASA's Ames Research Center. The spacecraft is of a novel design (a spacecraft bus never previously flown)—and of much lower cost than typical NASA science missions—which presented novel challenges to the trajectory design team in getting the new spacecraft launched to the Moon with a high-confidence spaceflight trajectory plan, while dealing with a first-use new rocket (Minotaur V) and a spacecraft with no flight test legacy. (see Lunar transit, below.) LADEE mission makes use of the Modular Common Spacecraft Bus, or body, made of a lightweight carbon composite with an unfueled mass of 547.2 pounds. The bus has the ability to perform on various kinds of missions - including voyages to the Moon and Near-Earth objects- with different modules or applicable systems. This modular concept is an innovative way of transitioning away from custom designs and toward multi-use designs and assembly-line production, which could drastically reduce the cost of spacecraft development. The LADEE spacecraft bus modules consist of the Radiator Module, that carries the avionics, electrical system, and attitude sensors; the Bus Module; the Payload Module that carries the two largest instruments, and the Extension Modules, which house the propulsion system.
The main structure is 2.37 m (7.8 ft) high, 1.85 m (6.1 ft) wide and 1.85 m (6.1 ft) deep. The total mass of the spacecraft is 383 kg (844 lb).
Electric power is generated by a photovoltaic system composed of 30 panels of silicon solar cells producing 295 W at one AU. The solar panels are mounted on the satellite's exterior surfaces and the electrical power is stored in one lithium-ion battery providing up to 24 amp-hours of 28-volt power.
The LADEE propulsion system consists of an orbit control system (OCS) and a reaction control system (RCS). The OCS provides velocity control along the +Z axis for large velocity adjustments. The RCS provides three-axis attitude control during burns of the OCS system, and will also provide momentum dumps for the reaction wheels which are the primary attitude control system between OCS burns.
The main engine is a 455N High Performance Apogee Thruster (HiPAT). The high efficiency 22N attitude control thrusters are manufactured using high temperature materials and similar to the HiPAT. The main engine provides the majority of the thrust for spacecraft trajectory correction maneuvers. The control system thrusters will be used for the small maneuvers planned for the science phase of the mission.
Following the science phase, a decommissioning period is planned, during which the altitude will be managed down to lower altitude and the spacecraft will impact the lunar surface.
LADEE carries three science instruments and a technology demonstration.
The science payload consists of:
- Neutral Mass Spectrometer (NMS), that will perform in situ measurements of exospheric species. The instrument has heritage from the SAM instrument on the Mars Science Laboratory.
- UV-Vis Spectrometer (UVS), that will measure both the dust and exosphere. The instrument has heritage from the UV-Vis spectrometer on the LCROSS mission.
- Lunar Dust EXperiment (LDEX), that will directly measure dust. The instrument has heritage from instruments on Galileo, Ulysses and Cassini.
- LADEE also carries a technology demonstration payload for testing an optical communication system. The Lunar Laser Communication Demonstration (LLCD) will use a laser to transmit and receive data as pulses of light, much the same as data is transferred in a fiber optic cable, to three ground stations. This method of communication has the potential to provide five times the current data return, as compared to radio frequency communication, from both LADEE and future missions. The technology is a direct predecessor to NASA's Laser Communications Relay Demonstration (LCDR) system due to launch in 2017.
The LADEE science teams continue to analyze data acquired at the time of the Chang'e 3 landing on 14 December 2013.
- The Lunar Dust EXperiment (LDEX) team noted an increase in dust around the time of the landing. However, the rise preceded the landing time by many hours, suggesting a different origin. Indeed, the Geminid meteor shower coincided with this landing event and produced elevated dust counts before, during and after the landing period. The team reported that "if LADEE did encounter any lunar soil particles thrown up by the final descent of Chang'e 3, they would have been lost in the background of Geminid-produced events."
- The Neutral Mass Spectrometer (NMS) team has been searching the data for exhaust gas species such as water, carbon monoxide and carbon dioxide (CO and CO2) as well as nitrogen (N2).
- The Ultraviolet and Visible light Spectrometer (UVS) carried out a series of before/after observations looking for effects of both the landing and meteor showers. Analysis revealed an increase in sodium in the exosphere in connection with the Geminid meteor shower, as well as evidence of increased light scattering due to dust. The UVS also has been monitoring emission lines of atomic oxygen, and has seen emissions that may indicate the presence of both iron (Fe) and titanium (Ti), which were expected but they have never before been observed.
The team for LADEE includes contributors from NASA Headquarters, Washington D.C., NASA's Ames Research Center, Moffett Field, California, NASA’s Goddard Space Flight Center, Greenbelt, Maryland, and the Laboratory for Atmospheric and Space Physics at the University of Colorado at Boulder. Guest investigators include those from the University of California, Berkeley;The Johns Hopkins University Applied Physics Laboratory, Laurel, Maryland; the University of Colorado; the University of Maryland; and NASA's Goddard Space Flight Center, Greenbelt, Maryland.
LADEE in August 2013, prior to being encapsulated into its fairing
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|Wikimedia Commons has media related to LADEE.|
- NASA's LADEE Mission site
- LADEE at NASA Science
- MIT's Lincoln Lab, lasercomm terminal development
- NASA's Lunar Science Program - February 27, 2008 - Kelly Snook
- Overview for K-8 students (YouTube video)