''Schiaparelli'' EDM () was a failed Entry, Descent, and Landing Demonstrator Module (EDM) of the
ExoMars
ExoMars (Exobiology on Mars) is an astrobiology programme of the European Space Agency (ESA).
The goals of ExoMars are to search for signs of past life on Mars, investigate how the Martian water and geochemical environment varies, investigate ...
programme—a joint mission of the
European Space Agency
The European Space Agency (ESA) is a 23-member International organization, international organization devoted to space exploration. With its headquarters in Paris and a staff of around 2,547 people globally as of 2023, ESA was founded in 1975 ...
(ESA) and the Russian Space Agency
Roscosmos
The State Corporation for Space Activities "Roscosmos", commonly known simply as Roscosmos (), is a State corporation (Russia), state corporation of the Russian Federation responsible for space science, space flights, List of space agencies, c ...
. It was built in Italy and was intended to test technology for future soft landings on the surface of
Mars
Mars is the fourth planet from the Sun. It is also known as the "Red Planet", because of its orange-red appearance. Mars is a desert-like rocky planet with a tenuous carbon dioxide () atmosphere. At the average surface level the atmosph ...
. It also had a limited but focused science payload that would have measured atmospheric electricity on Mars and local meteorological conditions.
Launched together with the
ExoMars Trace Gas Orbiter
The ExoMars Trace Gas Orbiter (TGO or ExoMars Orbiter) is a collaborative project between the European Space Agency (ESA) and the Russian Roscosmos agency that sent an atmospheric research orbiter and the ''Schiaparelli'' demonstration lande ...
(TGO) on 14 March 2016, ''Schiaparelli'' attempted a landing on 19 October 2016. Telemetry signals from ''Schiaparelli'', monitored in real time by the Giant Metrewave Radio Telescope in India (and confirmed by ''
Mars Express
''Mars Express'' is a space exploration mission by the European Space Agency, European Space Agency (ESA) exploring the planet Mars and its moons since 2003, and the first planetary mission attempted by ESA.
''Mars Express'' consisted of two ...
''), were lost about one minute from the surface during the final landing stages. On 21 October 2016, NASA released an image by the '' Mars Reconnaissance Orbiter'' showing what appears to be the lander's crash site. The telemetry data accumulated and relayed by ESA's
ExoMars Trace Gas Orbiter
The ExoMars Trace Gas Orbiter (TGO or ExoMars Orbiter) is a collaborative project between the European Space Agency (ESA) and the Russian Roscosmos agency that sent an atmospheric research orbiter and the ''Schiaparelli'' demonstration lande ...
and ''
Mars Express
''Mars Express'' is a space exploration mission by the European Space Agency, European Space Agency (ESA) exploring the planet Mars and its moons since 2003, and the first planetary mission attempted by ESA.
''Mars Express'' consisted of two ...
'' were used to investigate the failure modes of the landing technology employed.
Namesake
The ''Schiaparelli'' Entry, Descent, and Landing Demonstrator module is named for Giovanni Schiaparelli (1835–1910), an astronomer active in the 19th century who made Mars observations. In particular, he recorded features he called ''canali'' in his native Italian. His observations of what translates as channels in English inspired many. The dark streaks on Mars are an
albedo
Albedo ( ; ) is the fraction of sunlight that is Diffuse reflection, diffusely reflected by a body. It is measured on a scale from 0 (corresponding to a black body that absorbs all incident radiation) to 1 (corresponding to a body that reflects ...
feature which is related to dust distribution; these albedo features on Mars slowly change over time, and in the last few decades have been monitored by Mars orbiters. Schiaparelli is famous for making hand-drawn maps of Mars during its 1877 oppositions with Earth with an optical refracting telescope. He was also the first astronomer to determine the relationship between comet debris and yearly meteor showers.
Other things named for Schiaparelli include the main-belt asteroid 4062 Schiaparelli, named on 15 September 1989 (), the lunar crater Schiaparelli, the Martian crater Schiaparelli, Schiaparelli Dorsum on Mercury, and the 2016
ExoMars
ExoMars (Exobiology on Mars) is an astrobiology programme of the European Space Agency (ESA).
The goals of ExoMars are to search for signs of past life on Mars, investigate how the Martian water and geochemical environment varies, investigate ...
EDM lander.
The mission was named in November 2013; previously it was known as the Exomars Entry, descent and landing Demonstrator Module, or ExoMars EDM for short. Another name was ExoMars ''static lander'', however some designs for what was the static lander are quite different due to various stages of design and program restructuring. Another name, especially for both orbiter and lander together is ''ExoMars 2016''.
Origins and development
The EDM traces itself back to the ESA Aurora programme, which has the goal of human exploration of space, and thus producing missions that are building blocks to support this goal. ExoMars originated out of this, and provides context for understanding the EDM. Schiaparelli forms an important "block" of learning how to land heavy payloads on Mars, which is vital to future crewed missions. Another "block" is the ExoMars rover, which is intended to demonstrate among other things the ability to traverse several km/miles on the surface of Mars. The Aurora program is focused on two types of the mission, one are larger flagship spacecraft and the other are smaller missions specifically meant to offload risk from the larger missions.
In 2005 the ESA council approved 650 million Euros for a Mars rover and static lander. At this time the idea was for a single launch bringing both a
Mars Exploration Rover
NASA's Mars Exploration Rover (MER) mission was a robotic space mission involving two Mars rovers, ''Spirit (rover), Spirit'' and ''Opportunity (rover), Opportunity'', exploring the planet Mars. It began in 2003 with the launch of the two rove ...
class rover and instrumented static lander to Mars with a simpler cruise stage;in this case the static lander both landed the rover and performed its own studies. However to accomplish its mission goals within the constraints of using a Soyuz rocket for launch, the rover was budgeted for just 6 kg. To enable a larger rover, the Ariane V,
Atlas V
Atlas V is an expendable launch system and the fifth major version in the Atlas (rocket family), Atlas launch vehicle family. It was developed by Lockheed Martin and has been operated by United Launch Alliance (ULA) since 2006. Primarily used to ...
, and Proton were evaluated. Rovers from 180 kg up to 600 kg were considered, and eventually the idea of test lander to offload risk from the rover lander arose, which fitted well with a two-launch strategy allowing a heavier orbiter and a heavier rover on the second launch.
Early in development, the lander was to be carried by a dedicated cruise stage called the ''Carrier Module''. Eventually, the Trace Gas Orbiter mission was merged into ExoMars, becoming the carrier for the EDM.
Overview
Although the lander crashed, the data transmitted from ''Schiaparelli'' are expected to provide ESA and Roscosmos with the technology for landing on the surface of Mars with a controlled soft landing. This technology will be used by the ''Rosalind Franklin'' rover, part of the
ExoMars
ExoMars (Exobiology on Mars) is an astrobiology programme of the European Space Agency (ESA).
The goals of ExoMars are to search for signs of past life on Mars, investigate how the Martian water and geochemical environment varies, investigate ...
programme, which was due to launch in 2022. The rovers' launch has been delayed as a consequence of the
Russian invasion of Ukraine
On 24 February 2022, , starting the largest and deadliest war in Europe since World War II, in a major escalation of the Russo-Ukrainian War, conflict between the two countries which began in 2014. The fighting has caused hundreds of thou ...
. In July 2022, ESA terminated its cooperation on the project with Russia. , the launch of the rover is not expected to occur before 2028 due to the need for a new non-Russian landing platform.
Pre-launch
The descent module ''Schiaparelli'' and orbiter completed testing and were integrated to a Proton-M rocket at the
Baikonur cosmodrome
The Baikonur Cosmodrome is a spaceport operated by Russia within Kazakhstan. Located in the Kazakh city of Baikonur, it is the largest operational space launch facility in terms of area. All Russian Human spaceflight, crewed spaceflights are l ...
in
Baikonur
Baikonur ( ; ) is a city in Kazakhstan on the northern bank of the Syr Darya river. It is currently leased and administered by the Russian Federation as an enclave until 2050. It was constructed to serve the Baikonur Cosmodrome with adminis ...
in mid-January 2016. TGO and EDM arrived at Baikonur in December 2015. In February the spacecraft was mounted to the Briz-M upper stage, and in early March that was attached to the Proton rocket.
Liftoff
The launch occurred at 09:31 GMT (15:31 local time) on 14 March 2016. Four rocket burns occurred in the following 10 hours before the descent module and orbiter were released. A signal from the orbiter was received at 21:29 GMT that day, confirming that the launch was successful and the spacecraft was functioning properly. Shortly after separation from the probes, the Briz-M upper booster stage exploded a few kilometres away, without damaging the orbiter or lander.
Cruise, separation and arrival
After its launch, the Trace Gas Orbiter (TGO) and EDM traveled together coasting through space towards Mars. During this time the EDM was powered from an umbilical power line to the TGO, thus preserving the EDM's limited internal batteries. A deep space manoeuvre was executed by the TGO main engine in two legs on 28 July and on 11 August in order to target the entry flight path angle and the landing site. On 14 October 2016, the TGO did a final adjustment to its trajectory before the separation of Schiaparelli. The launch mass of the two spacecraft together is 4332 kg including the 600 kg ''Schiaparelli'' module. This was the heaviest spacecraft yet sent to Mars. The journey from Earth to Mars in 2016 took about 7 months.
On 16 October 2016, the TGO and EDM separated, the orbiter heading for Mars orbit insertion and the EDM for Mars atmospheric entry. Prior to the separation, the EDM was spun up 2.5 RPM (see also spin stabilization) and then released at a velocity of about 1 km/h relative to TGO. The EDM was designed to go into a lower-power hibernation mode for about 3 days while it traveled solo to Mars. The EDM came out of hibernation about an hour and a half prior to reaching the Martian atmosphere. Meanwhile, after the separation, the TGO adjusted its trajectory for its Mars orbit insertion and by 19 October 2016 performed a 139-minute rocket engine burn to enter Mars orbit. On the same day, the ''Schiaparelli'' module arrived at Mars traveling at and engaged in its prime task of entry, descent, and landing. After a successful atmospheric entry, the module's speed was reduced from the 5.8 km/s entry value to a few hundred m/s due to the drag force provided by the
atmosphere of Mars
The atmosphere of Mars is the layer of gases surrounding Mars. It is primarily composed of carbon dioxide (95%), molecular nitrogen (2.85%), and argon (2%). It also contains trace levels of water vapor, oxygen, carbon monoxide, hydrogen, and nob ...
. During this phase of the flight, a heat shield was used to protect the payload from the severe heat load. The parachute was triggered by the on-board software when the
accelerometer
An accelerometer is a device that measures the proper acceleration of an object. Proper acceleration is the acceleration (the rate of change (mathematics), rate of change of velocity) of the object relative to an observer who is in free fall (tha ...
s detected a given non-gravitational acceleration value of 9 m/s2, as expected. After having reached the sub-sonic regime by means of the nominally-inflated parachute, the ''Schiaparelli'' module experienced an anomaly causing the backshell and parachute release to occur earlier than expected and preventing the retrorockets from slowing the descent. The hard touch-down location, reconstructed using data from the Mars Reconnaissance Orbiter, was identified quite close to the expected landing site, about 6.4 km short-range from it. The TGO entered Mars' orbit and it underwent several months of aerobraking to adjust its speed and orbit, with science activities beginning in late 2017. The TGO will continue serving as a relay satellite for future
Mars landing
A Mars landing is a landing of a spacecraft on the surface of Mars. Of multiple attempted Mars landings by robotic spacecraft, robotic, uncrewed spacecraft, ten have had successful soft landings. There have also been studies for a possible huma ...
missions until 2022. (PDF)
Landing site
The landing site chosen was Meridiani Planum, a Martian plain prized by Mars landers for its flat terrain and low elevation that gives a spacecraft time and distance to slow down before reaching the ground. The EDM cannot avoid obstacles during its descent, so it was important to pick a large flat area with a minimum of obstacles. The landing ellipse is about 100 km long by 15 km wide, centered at 6° west and 2° south running east–west, with the eastern edge including the ''Opportunity'' rover landing site, and near Endeavour crater where it was still operating when the EDM was launched and when it attempted to land. The ''Opportunity'' rover (MER-B) landing site is called the ''Challenger Memorial Station''. It was also thought that the EDM would have a chance of arriving when Mars experienced its global dust storms, and thus gain knowledge about the atmosphere under these less common conditions. The site is also known to be scientifically interesting; the ''Opportunity'' rover discovered a type of iron mineral that forms in the presence of water, so it is theorized there was a significant amount of water there in the past.
Dust storm goal
The landing was planned to take place on
Meridiani Planum
Meridiani Planum (alternatively Terra Meridiani) is a large plain straddling the equator of Mars. The plain sits on top of an enormous body of sediments that contains bound water. The iron oxide in the spherules is crystalline (grey) hematite (Fe ...
during the dust storm season, which would have provided a chance to characterise a dust-loaded atmosphere during entry and descent, measure the dust's
static electricity
Static electricity is an imbalance of electric charges within or on the surface of a material. The charge remains until it can move away by an electric current or electrical discharge. The word "static" is used to differentiate it from electric ...
charge—typically produced by charge transfer on contact between particles—and to conduct surface measurements associated with a dust-rich environment.
Global dust storms have occurred at least nine times since 1924 including 1977, 1982, 1994, 2001 and 2007; the 2007 dust storms nearly ended the functioning of the solar-powered U.S. Mars Exploration Rovers ''Spirit'' and ''Opportunity''. Global dust storms obscured Mars when the ''
Mariner 9
Mariner 9 (Mariner Mars '71 / Mariner-I) was a robotic spacecraft that contributed greatly to the exploration of Mars and was part of the NASA Mariner program. Mariner 9 was launched toward Mars on May 30, 1971, from Spaceport Florida Launch Comp ...
'' orbiter arrived there in 1971, and it took several weeks for the dust to settle down and allow for clear imaging of the surface of Mars. It was predicted that Mars global dust storms were likely to occur in the fall of 2016, but they had not started when the EDM attempted its landing. Global dust storms hit in the summer of 2018, cutting off light to the solar powered
Opportunity rover
''Opportunity'', also known as MER-B (Mars Exploration Rover – B) or MER-1, and nicknamed Oppy, is a Robotics, robotic rover (space exploration), rover that was active on Mars from 2004 until 2018. ''Opportunity'' was operational on Mars for ...
which was still operating nearby to the Schiaparelli landing site.
Entry, descent, and landing events sequence
The ''Schiaparelli'' lander separated from the TGO orbiter on 16 October 2016, three days before arrival at Mars, and entered the atmosphere at on 19 October 2016 (see also
Mars atmospheric entry
Mars atmospheric entry is the atmospheric entry, entry into the atmosphere of Mars. High velocity entry into Martian air creates a CO2-N2 plasma, as opposed to O2-N2 for Earth air. ''Schiaparelli'' came out of hibernation several hours before its entry, at a speed of and an altitude of above the surface of Mars. The heat shield was used during the plunge into the atmosphere to decelerate the lander to by the time it reached altitude. During entry the COMARS+ instrumentation the EDM operated to collect data on how heat and air flow around the entry capsule.
After slowing its initial entry through the atmosphere, the module deployed a parachute and was to complete its landing on retrorockets by using a closed-loop guidance, navigation and control system based on a Doppler
radar altimeter
A radar altimeter (RA), also called a radio altimeter (RALT), electronic altimeter, reflection altimeter, or low-range radio altimeter (LRRA), measures altitude above the terrain presently beneath an aircraft or spacecraft by timing how long it t ...
sensor, and on-board
inertial measurement unit
An inertial measurement unit (IMU) is an electronic device that measures and reports a body's specific force, angular rate, and sometimes the Orientation (geometry), orientation of the body, using a combination of accelerometers, gyroscopes, an ...
s. Throughout the descent, various sensors recorded a number of atmospheric parameters and lander performance. The plan was that at in altitude the front heat shield would be jettisoned and the radar altimeter turned on, then at altitude above Mars the rear heat cover and parachute would be jettisoned.
The final stages of the landing were to be performed using pulse-firing liquid-fuel engines or retrorockets. About two metres above ground, the engines were designed to turn off and let the platform land on a crushable structure, designed to deform and absorb the final touchdown impact. On final landing it was designed to endure rocks about high, and it was hoped, but not guaranteed, that no out-sized boulders or craters would be encountered. On final contact, the lander was designed to handle slopes of up to 19 degrees and rocks up to in height.
The ''Opportunity'' rover was operating in the region and the two teams worked together to attempt to image the EDM on its descent, which, depending on conditions, might have been possible especially if the EDM "went long" in its landing ellipse. However, the rover's cameras had no view of the lander during its descent. It was the first time a surface probe attempted to image the landing of another vehicle from the surface of Mars. (Other spacecraft have imaged each other, especially orbiters viewing ones on the ground, and in 2005 ''Mars Global Surveyor'' imaged ''Mars Express'' in orbit around Mars.)
EDL summary (as planned):
Contact was lost with the module 50 seconds before the planned touch-down. By 21 October 2016, after studying the data, ESA said it was likely that things went wrong when the parachute released early, the engines then turned on but then turned off after too short a time.
Crash
The ''Schiaparelli'' lander attempted an automated landing on 19 October 2016, but the signal was unexpectedly lost a short time before the planned landing time. ESA's ''
Mars Express
''Mars Express'' is a space exploration mission by the European Space Agency, European Space Agency (ESA) exploring the planet Mars and its moons since 2003, and the first planetary mission attempted by ESA.
''Mars Express'' consisted of two ...
'' and NASA's '' Mars Reconnaissance Orbiter'' (MRO) and MAVEN continued listening for the lander's signal to no avail.
''Schiaparelli'' transmitted about 600 megabytes of telemetry during its landing attempt, and detailed analysis found that its atmospheric entry occurred normally, with the parachute deploying at and , and its heat shield releasing at . However, the lander's
inertial measurement unit
An inertial measurement unit (IMU) is an electronic device that measures and reports a body's specific force, angular rate, and sometimes the Orientation (geometry), orientation of the body, using a combination of accelerometers, gyroscopes, an ...
, which measures rotation, became saturated (unable to take higher readings) for about one second. This saturation, coupled with data from the navigation computer, generated an altitude reading that was negative, or below ground level. This caused the premature release of the parachute and back shell. The braking thrusters then fired for about three seconds rather than the expected 30 seconds, followed by the activation of ground systems as if the vehicle had already landed. In reality, it was still at an altitude of . The lander continued transmitting for 19 seconds after the thrusters cut off; the loss of signal occurred 50 seconds before it was supposed to land. ''Schiaparelli'' impacted the Martian surface at , near terminal velocity.
A day after the attempted landing, the Context Camera of NASA's MRO identified new ground markings due to the lander's impact and parachute. The crash site is about 54 km (~33.5 miles) from where the active NASA Mars rover ''Opportunity'' was at the time of the landing. On 27 October 2016, ESA released high resolution images of the crash site taken by the MRO
HiRISE
High Resolution Imaging Science Experiment is a camera on board the '' Mars Reconnaissance Orbiter'' which has been orbiting and studying Mars since 2006. The 65 kg (143 lb), US$40 million instrument was built under the direction ...
camera on 25 October 2016. The front heatshield, module impact site, and the rear heat-shield and parachute are identified. It is thought that the crater is about half a metre (yard) deep and it may be possible to further study this crater at a later time. On a related note, an artificially made crater was actually the goal of the ''THOR'' mission proposed under the Mars Scout program that produced Phoenix and MAVEN, the goal was sub-surface excavation. That mission was passed over, but another orbiter was able to discover naturally occurring fresh impact craters, and ice was found in them.
Although the lander crashed, ESA officials declared ''Schiaparelli'' a success because it had fulfilled its primary function of testing the landing system for the then-planned 2020 ''
Kazachok
The ExoMars ''Kazachok'' (; formerly ExoMars 2020 Surface Platform) was a planned robotic Mars lander led by Roscosmos, part of the ExoMars 2022 joint mission with the European Space Agency. ''Kazachok'' translates as "Little Cossack", and is ...
'' lander and returning telemetry data during its descent. By 20 October, the bulk of the descent data had been returned to Earth and was being analysed. Unlike the '' Beagle 2'' lander, which was not heard from again after being released from ''Mars Express'' in 2003, the Exomars module transmitted during descent so data collected and transmitted on the way down was not lost if the spacecraft was destroyed on impact.
Investigation into cause of the crash
An investigation that concluded in May 2017 identified four "root causes for the mishap .. Insufficient uncertainty and configuration management in the modelling of the parachute dynamics which led to expect much lower dynamics than observed in flight;
Inadequate persistence time of the IMU nertial Measurement Unitsaturation flag and inadequate handling of IMU saturation by the GNC uidance Navigation and Control Insufficient approach to Failure Detection, Isolation and Recovery and design robustness; Mishap in management of subcontractors and acceptance of hardware."
The board of inquiry's investigation revealed that at the time that the lander deployed its parachute it began spinning unexpectedly fast. This superfast rotation briefly saturated ''Schiaparelli'' spin-measuring instrument, which resulted in a large attitude-estimation error by the guidance, navigation and control-system software. This resulted in the computer calculating that it was below ground level, triggering the early release of the parachute and backshell, a brief firing of the thrusters for only 3 seconds instead of 30 seconds, and the activation of the on-ground system as if ''Schiaparelli'' had landed. The inquiry also determined that " e mission would not have been jeopardised by the attitude knowledge error induced by IMU nertial Measurement Unitsaturation, if the persistence time would have been set at a lower value."
Images of module's crash site suggested that a fuel tank may have exploded in the impact. It is estimated that the lander impacted the surface at about . Additional imaging of the site by November further confirmed the identity of the spacecraft's parts. The additional imaging was in colour and it was noted that parachute was slightly shifted.
By taking more images using a technique called super-resolution reconstruction (SRR) the resolution can be improved, and this was done for the formerly lost Beagle 2 probe. Two other benefits to more images is that is easier to discern between image noise such as cosmic ray hits and real objects, and among bright spots high albedo objects versus momentary specular reflections. Finally, with multiple images over time, movement and changes, such as the wind blowing a parachute can be observed.
Instrument and sensor payload
The primary mission goal was to test the landing systems, including the parachute, Doppler radar altimeter,
hydrazine
Hydrazine is an inorganic compound with the chemical formula . It is a simple pnictogen hydride, and is a colourless flammable liquid with an ammonia-like odour. Hydrazine is highly hazardous unless handled in solution as, for example, hydraz ...
thrusters, etc. The secondary mission goal was scientific. The lander was to measure the wind speed and direction, humidity, pressure and surface temperature, and determine the transparency of the atmosphere. The surface science payload was called DREAMS, and was designed to obtain meteorological data for a few days after landing, as well as make the first measurements of
atmospheric electricity
Atmospheric electricity describes the electrical charges in the Earth's atmosphere (or that of another planet). The movement of charge between the Earth's surface, the atmosphere, and the ionosphere is known as the global atmospheric electrica ...
on Mars.
A descent camera (DECA) was included in the payload. Its captured images were to be transmitted after landing. AMELIA, COMARS+, and DECA collected data during the entry, descent, and landing for about six minutes. Much of this data was transmitted while it was descending. Although EDL portion was designed to last literally a few minutes, and the surface observations at most a few days, one instrument, INRRI, was a passive laser retro-reflector that could be used as long as possible, even decades later, for laser range-finding of the lander.
INRRI was mounted to the top (zenith) side of the lander, to enable spacecraft above to target it. Its mass was about 25 grams, and it was contributed by the Italian Space Agency (ASI). The design used a cube corner reflector to return incoming laser light. The cubes are made of fused silica which are mounted to an aluminum support structure. INRRI was also mounted to the
InSight
Insight is the understanding of a specific causality, cause and effect within a particular context. The term insight can have several related meanings:
*a piece of information
*the act or result of understanding the inner nature of things or of se ...
Mars lander.
;Summary of the science-technology payload:
*DREAMS (Dust Characterization, Risk Assessment, and Environmental Analyser on the Martian Surface)
**MetWind (wind detection)
**DREAMS-H (humidity detection)
**DREAMS-P (pressure detection)
**MarsTem (temperature detection)
**Solar Irradiance Sensor (transparency of the atmosphere)
**Micro-ARES (atmospheric electricity detector)
*AMELIA (Atmospheric Mars Entry and Landing Investigation and Analysis)
*DECA (Descent Camera)
*COMARS+ (Combined Aerothermal Sensor Package)
**Measured heat during Mars atmospheric entry.
*INRRI (INstrument for landing – Roving laser Retroreflector Investigations)
**Compact laser retro-reflector for detecting the lander by laser-ranging
DREAMS
The lander's scientific payload for the surface was the meteorological DREAMS (Dust Characterization, Risk Assessment, and Environment Analyser on the Martian Surface) package, consisting of a suite of sensors to measure the wind speed and direction (MetWind), humidity (MetHumi), pressure (MetBaro), surface temperature (MarsTem), the transparency of the atmosphere (Solar Irradiance Sensor – SIS), and atmospheric electrification (Atmospheric Relaxation and Electric-field Sensor – Micro-ARES).F. Esposito, ''et al.,' "DREAMS for the ExoMars 2016 mission: a suite of sensors for the characterization of Martian environment" (PDF). European Planetary Science Congress 2013, EPSC Abstracts Vol. 8, EPSC2013-815 (2013) The institutions that contributed to the DREAMS science payload include INAF and CISAS from Italy, LATMOS from France,
ESTEC
The European Space Research and Technology Centre (ESTEC) is the European Space Agency's main technology development and test centre for spacecraft and space technology. It is situated in Noordwijk, South Holland, in the western Netherlands, alth ...
INTA
Inta (, ) is a types of inhabited localities in Russia, town in the Komi Republic, Russia. Population:
History
Inta was founded around 1940 as a settlement to support a geological expedition to explore coal deposits and projecting of mines. The ...
from Spain.
The DREAMS payload was intended to function for 2 to 8 Mars days as an environmental station for the duration of the surface mission after landing. The planned lander arrival was made to coincide with the Mars global dust storm season and collect data on a dust-loaded Mars atmosphere. DREAMS had been hoped to provide new insights into the role of electric forces on dust lifting, the mechanism that initiates dust storms. In addition, the MetHumi sensor was intended to complement MicroARES measurements with critical data about humidity, to enable scientists to better understand the dust electrification process.
Atmospheric electricity
Atmospheric electricity describes the electrical charges in the Earth's atmosphere (or that of another planet). The movement of charge between the Earth's surface, the atmosphere, and the ionosphere is known as the global atmospheric electrica ...
on Mars is still unmeasured, and its possible role in dust storms and atmospheric chemistry remains unknown. It has been speculated that atmospheric electricity may have played a role in the inconclusive results from the ''Viking'' lander life experiments, which were positive for metabolizing microbial life, but no organic compounds were detected by the mass spectrometer. The two favored possible explanations are reactions with
hydrogen peroxide
Hydrogen peroxide is a chemical compound with the formula . In its pure form, it is a very pale blue liquid that is slightly more viscosity, viscous than Properties of water, water. It is used as an oxidizer, bleaching agent, and antiseptic, usua ...
or
ozone
Ozone () (or trioxygen) is an Inorganic compound, inorganic molecule with the chemical formula . It is a pale blue gas with a distinctively pungent smell. It is an allotrope of oxygen that is much less stable than the diatomic allotrope , break ...
created by
ultraviolet light
Ultraviolet radiation, also known as simply UV, is electromagnetic radiation of wavelengths of 10–400 nanometers, shorter than that of visible light, but longer than X-rays. UV radiation is present in sunlight and constitutes about 10% of th ...
or atmospheric electrical processes during dust storms.
DREAMS-P was a pressure sensor and DREAMS-H was for humidity; the sensors feed a single data-handling circuit board.
In addition to the surface payload, a camera called DECA (Descent Camera) on the lander operated during the descent. It was intended to deliver additional context information and exact location data in the form of images. DECA is a reflight of the Visual Monitoring Camera (VMC) of the Planck and Herschel mission.
Another surface experiment that was focused on dust was the Materials Adherence Experiment on the
Mars Pathfinder
''Mars Pathfinder'' was an American robotic spacecraft that landed a base station with a rover (space exploration), roving probe on Mars in 1997. It consisted of a Lander (spacecraft), lander, renamed the Carl Sagan Memorial Station, and a ligh ...
lander, about twenty years prior to ExoMars.
Descent Camera
The Descent Camera (DECA) was intended to capture about 15 downward-looking views as it approached the surface of Mars. It was to begin acquiring images after the lower heat shield was ejected. This camera had a 60 degree field of view to capture
greyscale
In digital photography, computer-generated imagery, and colorimetry, a greyscale (more common in Commonwealth English) or grayscale (more common in American English) image is one in which the value of each pixel is a single sample repres ...
images, to support technical knowledge of the descent. DECA was a flight spare of the visual monitoring camera of the
Herschel Space Observatory
The Herschel Space Observatory was a space observatory built and operated by the European Space Agency (ESA). It was active from 2009 to 2013, and was the largest infrared telescope ever launched until the launch of the James Webb Space Telesco ...
and Plank mission that were launched together. The camera dimensions are squared, with a mass of . The DECA descent camera data were stored during descent and not meant to be relayed to Earth until after landing, so these images were lost in the crash. The purpose of this transfer delay was to protect the spacecraft and data from electrostatic discharges. DECA was designed and built in Belgium by ''Optique et Instruments de Précision'' (OIP).
The main goals for DECA included:
*image landing area
*measure transparency of the Martian atmosphere,
*collect data for 3-D
topography
Topography is the study of the forms and features of land surfaces. The topography of an area may refer to the landforms and features themselves, or a description or depiction in maps.
Topography is a field of geoscience and planetary sci ...
of landing area
Preliminary results
Because the ''Schiarapelli'' demonstrator lander transmitted ''during'' its descent, a great deal of telemetry was successfully returned. About 600 megabytes of data, amounting to about 80% of telemetry, were relayed to Earth were used to investigate the failure modes of the landing technology employed.
Specifications
Note about masses: on the Mars surface the gravity is less than on Earth, so the weight is 37% of the Earth weight.
Power systems
At one point, Roscosmos offered to contribute a 100 watt
radioisotope thermoelectric generator
A radioisotope thermoelectric generator (RTG, RITEG), or radioisotope power system (RPS), is a type of nuclear battery that uses an array of thermocouples to convert the Decay heat, heat released by the decay of a suitable radioactive material i ...
(RTG) power source for the EDM lander to allow it to monitor the local surface environment for a full Martian year, but because of complex Russian export control procedures, it later opted for the use of a non-rechargeable electric battery with enough power for 2 to 8 sols. Solar panels were also considered when a longer mission (1–2 months) supported by a heavier, more complex, lander was under consideration. By the 2010s the focus was on executing a short-lived (a few days surface time) technology demonstration, with an emphasis on landing systems.
Communication systems and network
''Schiaparelli'' had a UHF radio to communicate with Mars orbiters. The lander had two antennae, one on the back shell and one on the lander. When the back shell is ejected, it can transmit from the spiral antenna on body of the lander. When an orbiter can communicate with the lander depends on where it is in its orbit, and not all orbiters could record or talk with lander because the globe of Mars blocks the line of sight to the lander. The ExoMars TGO could also communicate with it using the UHF system. The EDM "woke up" from hibernation about 90 minutes prior to landing, and transmitted continuously for 15 minutes prior to landing.
During its landing, the EDM signal was monitored at Mars by the ''
Mars Express
''Mars Express'' is a space exploration mission by the European Space Agency, European Space Agency (ESA) exploring the planet Mars and its moons since 2003, and the first planetary mission attempted by ESA.
''Mars Express'' consisted of two ...
'' orbiter, and remotely by the Giant Metrewave Radio Telescope in Pune, India. ''Mars Express'' also communicates with other landers and rovers using its Melacom communication system. The '' Mars Reconnaissance Orbiter'' (MRO) overflew the landing two hours after landing, and was available to check for signals from ''Schiaparelli''. The ExoMars TGO could also communicate with it using the UHF system.
The communication system standard at Mars is the
Electra
Electra, also spelt Elektra (; ; ), is one of the most popular Greek mythology, mythological characters in tragedies.Evans (1970), p. 79 She is the main character in two Greek tragedies, ''Electra (Sophocles play), Electra'' by Sophocles and ''Ele ...
radio, in use since the arrival of the ''Mars Reconnaissance Orbiter'' in 2006. Prior to this, several orbiters used a first generation UHF relay system, including ''Mars Global Surveyor'', ''Mars Odyssey'', and ''Mars Express''. Using orbiters to relay data from Mars landers and rovers is noted for its energy efficiency.
On 19 October 2016 it took 9 minutes and 47 seconds for a radio transmission to travel at roughly the speed of light from Mars to Earth. So even though the radio array at Pune listened in "real time", the entire EDL sequence, which would take about 6 minutes, had already occurred even as it was being recorded as starting to enter the atmosphere. There is a tiny bit of variation because the speed of light is slowed down by the air of Mars and Earth (see
Refractive index
In optics, the refractive index (or refraction index) of an optical medium is the ratio of the apparent speed of light in the air or vacuum to the speed in the medium. The refractive index determines how much the path of light is bent, or refrac ...
), and another factor is
Time dilation
Time dilation is the difference in elapsed time as measured by two clocks, either because of a relative velocity between them (special relativity), or a difference in gravitational potential between their locations (general relativity). When unsp ...
, because the probe existed at a significantly different velocity and in a different gravitational field the radio station back on Earth (though relatively small).
Computing
The ''Schiaparelli'' lander has two main computers, one is called the Central Terminal & Power Unit (CTPU) and housed in a warm box on top, and the other computer is called the Remote Terminal & Power Unit (RTPU) and is on the underside of the lander."Schiaparelli Mars Lander (EDM)". ''Spaceflight101.com''. Retrieved: 27 October 2016. Overall, the CTPU handles surface operations and the RTPU handles entry and descent, and is actually destroyed on final landing with surface because it is on the underside. When the Trace Gas Orbiter and Entry Demonstrator Module are connected, the RTPU handles the interface and sends power from the orbiter to the module. When it disconnects from the orbiter, then it must run off its internal batteries. The CTPU uses a LEON central processor based on
Sun Microsystems
Sun Microsystems, Inc., often known as Sun for short, was an American technology company that existed from 1982 to 2010 which developed and sold computers, computer components, software, and information technology services. Sun contributed sig ...
' RISC-based SPARC processor architecture, and also has RAM, PROM, and a timer. The CTPU also handles data sent to the UHF radio communication system. When the lander disconnects from the orbiter, it spends most of its time in a low-power hibernation mode while it coasts through space before entering the Martian atmosphere. The lander must coast through space for about 3 days by itself before landing, meanwhile the orbiter has to do a Mars orbit insertion. The DECA descent camera data is not downloaded to the computer for relay to Earth until after landing, and it is not transmitted during descent.
Parachute
A disk-band-gap parachute was deployed by a pyrotechnic mortar. It was tested at full scale in the largest wind tunnel in the world as part of its development. A sub-scale parachute was tested in Earth's atmosphere in 2011; it was ascended by balloon to 24.5 kilometers altitude and then released, and the pyrotechnic deployment systems was tested after a period of free-fall. On 19 October 2016 the parachute was successfully deployed on Mars.
In the summer of 2019, problems with the parachute for the next tranche of the project occurred during testing, despite the EDM technology test; the issues with the parachute system may delay that phase.
Retro-rockets
''Schiaparelli'' module has 3 sets of three thrusters, nine total, that operate starting at about 1 km (half a mile) up in pulse mode, slowing the spacecraft from . Each of the nine engines is a CHT-400 rocket engine that can produce 400 Newtons of thrust. These rocket engines are fueled by three spherical 17.5 liter tanks holding hydrazine propellant. The tanks hold about 15–16 kilograms of hydrazine (about 34 pounds, 2.4 stones) of fuel per tank, or 46 kg overall (101 pounds or 7.24 stones). The propellant is pressurized by helium, held in a single tank containing 15.6 liters at a pressure of 170 bar (2465 psi). The thrusters shut down 1–2 meters/yards from the surface, after which the crumple zone underneath the lander handles the final stop. Data from a timer,
doppler radar
A Doppler radar is a specialized radar that uses the Doppler effect to produce velocity data about objects at a distance. It does this by bouncing a microwave signal off a desired target and analyzing how the object's motion has altered the fre ...
, and inertial measurement unit are merged in the lander's computers to control the operation of the thrusters.
Impact on ExoMars
A possible "shutdown" moment for the next ExoMars mission was the ESA ministerial meeting in December 2016 which considered certain issues including €300 million of ExoMars funding and lessons learned from the ExoMars 2016 missions so far. One concern was the ''Schiaparelli'' crash, as this landing system was to be used for the ExoMars 2020 mission consisting of the ''Rosalind Franklin'' rover delivered by the instrumented 2020 ''
Kazachok
The ExoMars ''Kazachok'' (; formerly ExoMars 2020 Surface Platform) was a planned robotic Mars lander led by Roscosmos, part of the ExoMars 2022 joint mission with the European Space Agency. ''Kazachok'' translates as "Little Cossack", and is ...
'' lander.
The ExoMars team has been praised for "putting a brave face" on what happened and being positive about the EDM's very credible return on its prime mission: data about entry, descent, and landing, despite the crash.
Another positive was the development of the demonstrator module as part of the overall grand plan for ExoMars, which meant that the landing technologies underwent a real-world test before carrying more valuable cargo.
A preliminary report on the malfunction was presented at the December 2016 ESA ministerial meeting. By December the outcome was known: ExoMars would go on being financially supported by the ESA. €436 million ($464 million) was authorized to finish the mission.
Glossary
*ASI: Agenzia Spaziale Italiana
*EDL: Entry, descent and landing
*EDM: EDL Demonstrator Module
*ESA: European Space Agency
*ESTEC: European Space Research and Technology Centre
*GMT: Greenwich Mean Time
*INAF: Istituto Nazionale di Astrofisica
*NASA: National Aeronautics and Space Administration
*Roscosmos: the Russian national space programme
*TGO:
Trace Gas Orbiter
The ExoMars Trace Gas Orbiter (TGO or ExoMars Orbiter) is a collaborative project between the European Space Agency (ESA) and the Russian Roscosmos agency that sent an atmospheric research orbiter and the ''Schiaparelli'' demonstration lande ...