
Mars Exploration Hub
From Mariner 4's first flyby to Perseverance's sample cache — every orbiter, rover, lander, and flyby, cited to primary sources.
Six decades of Mars exploration in six eras — from the first grainy flyby images to the first rock cores awaiting return to Earth.
1962–1971
The first spacecraft attempts to reach Mars — mostly failures early on, with Mariner 4 delivering humanity's first close-up photographs in 1965. These 21 grainy images showed a cratered, apparently dead world and shaped a generation of expectations.
1971–2001
Mariner 9 became the first spacecraft to orbit another planet (1971) and produced the first global map of Mars, revealing Olympus Mons and Valles Marineris. The Viking orbiters (1976) and Mars Global Surveyor (1997) refined our understanding of Martian geology, atmosphere, and potential past habitability.
1976–2008
Viking 1 and 2 achieved the first successful US landings (1976) and searched — inconclusively — for signs of life. Pathfinder (1997) proved modern landing systems. Phoenix (2008) confirmed water ice just below the surface at high latitudes. InSight (2018) listened to Marsquakes for the first time.
1997–present
Sojourner (1997) proved Mars roving was feasible. Spirit and Opportunity (2004) found definitive evidence of past liquid water. Curiosity (2012) confirmed ancient habitability at Gale Crater. Perseverance (2021) began caching samples and demonstrated oxygen production. Ingenuity proved powered flight on another world.
2020s–2030s
Perseverance's 24 cached sample tubes represent humanity's first step toward returning Mars material to Earth laboratories. Mars Sample Return (NASA-ESA) aims to retrieve these samples by the mid-2030s for definitive biosignature analysis that no rover instrument can match.
Status: Planning / Conceptual
2030s+
NASA's Moon-to-Mars roadmap and SpaceX's Starship architecture both target crewed Mars missions in the 2030s–2040s. Key unresolved challenges: transit radiation shielding, entry-descent-landing at scale, ISRU propellant production, and long-duration human health on a 26-month synodic cycle.
Status: Planning / Conceptual
Every surface vehicle sent to Mars — rovers, landers-with-mobility, and helicopters — cited to NASA JPL and agency primary sources.
Mars Pathfinder
Mars Exploration Rover — A
Mars Exploration Rover — B
Mars Science Laboratory
Mars 2020
Mars Helicopter Scout
Tianwen-1
Every orbital mission to Mars from the first global mapper to today's science relay fleet — sourced from NASA NSSDCA and agency primaries.
2001 Mars Odyssey
Sun-synchronous polar mapping orbit, ~400 km altitude, 2-hour period
THEMIS produced the first comprehensive global map of surface mineralogy, identifying volcanic and water-altered rock types across the entire planet
View mission →Highly elliptical polar orbit, 298 × 10,107 km, 6.72-hour period
MARSIS subsurface radar detected a 20 km wide subglacial liquid water lake under the south polar ice cap at ~1.5 km depth (published July 2018)
View mission →MRO
Nearly circular polar sun-synchronous orbit, ~300 km altitude, 112-minute period
HiRISE camera resolves surface features down to 25 cm — unprecedented resolution for any Mars mission and the benchmark for all subsequent landing site assessments
View mission →Mars Atmosphere and Volatile EvolutioN
Elliptical orbit, 145 × 6,200 km, 4.5-hour period; periodic deep-dip campaigns to ~125 km
Determined Mars loses approximately 100 grams of atmosphere per second to solar wind stripping via solar energetic particle events and coronal mass ejections
View mission →ExoMars 2016 / TGO
Near-circular polar science orbit, ~400 km altitude, 2-hour period
NOMAD and ACS instruments produced the most precise inventory of Martian trace gases to date, placing stringent upper limits on methane abundance (<0.05 ppb) — conflicting with earlier ESA/NASA detections and constraining possible biological or geological methane sources
View mission →Emirates Mars Mission (EMM)
Science orbit: 22,000 × 43,000 km elliptical, ~55-hour period
First spacecraft to capture a complete picture of Mars's atmospheric weather system within a single orbit due to its wide-area high-altitude vantage point
View mission →Tianwen-1
Relay/science orbit after lander separation: ~265 × 11,900 km elliptical
China's first Mars mission — made China the second nation to successfully land a rover on Mars (Zhurong, May 2021)
View mission →Elliptical, 1,387 × 17,144 km, 12-hour period
First spacecraft to orbit another planet — entered Mars orbit 1971-11-14
View mission →Viking 1
Elliptical polar orbit, 300 × 33,000 km, evolved over mission lifetime
Mapped 97% of the Martian surface at 200–300 m resolution — the first near-complete photographic atlas
View mission →Viking 2
Elliptical polar orbit; inclination raised to 75° to access higher latitudes
Imaged Utopia Planitia in detail to select the Viking 2 lander touchdown site
View mission →Never achieved orbit — contact lost during pre-orbit-insertion pressurization
No science data returned from Mars — contact lost August 21, 1993, three days before scheduled orbit insertion
View mission →MGS
Nearly circular polar mapping orbit, ~378 km altitude, 117-minute period
MOLA laser altimeter produced the most accurate global topographic map of any planet — revealing Mars is divided into two distinct hemispheres by elevation
View mission →Never achieved stable orbit — entered Martian atmosphere due to navigation error
No science data returned — spacecraft was destroyed on September 23, 1999 when it entered the Martian atmosphere
View mission →MOM / Mangalyaan
Highly elliptical, 421 × 80,000 km, 72.7-hour period
First Asian nation to reach Mars and the first Mars mission in history to succeed on its maiden attempt
View mission →Every surface mission to Mars — successful landers, landers lost in transit, and partial successes — cited to primary sources.
Viking 1
First successful soft landing in Mars history — and first to operate long-term on the surface
View mission →Viking 2
Second successful Mars soft landing, at the higher-latitude Utopia Planitia
View mission →Mars Pathfinder
First Mars lander using airbag-bounced landing — revolutionary entry, descent, and landing technology later adopted by MER rovers
View mission →Phoenix
Confirmed the presence of water ice just below the Martian surface at high latitudes — directly observed ice with the robotic arm
View mission →InSight (Interior Exploration using Seismic Investigations, Geodesy and Heat Transport)
Detected 1,319 Mars quakes over the mission lifetime, including magnitude-5.0 events — definitively proving Mars is seismically active
View mission →Tianwen-1
First Chinese successful Mars landing, making China only the third country (after the USSR and USA) to soft-land on Mars
View mission →Mars 3
Achieved the first soft landing on Mars on December 2, 1971
View mission →Mars Polar Lander
Never achieved surface operations — lost during entry, descent, and landing at the Martian south polar region on December 3, 1999
View mission →Beagle 2 (carried on Mars Express)
Confirmed by MRO HiRISE imagery in January 2015 to have landed successfully — 12 years after the mission was declared lost
View mission →ExoMars 2016 — Schiaparelli
Entry and descent systems partially successful — heatshield and parachute performed correctly through the initial phases
View mission →Government and multi-agency programs shaping Mars exploration — from NASA's long-running MEP to ESA's ExoMars and China's Tianwen campaign.
The UAE's Emirates Mars Mission (EMM, 'Hope' probe / Al-Amal) made the United Arab Emirates the first Arab nation to reach Mars when it entered orbit on February 9, 2021 — at a total programme cost reported in the region of $200M [1][2]. The follow-on Emirates Mission to the Asteroid Belt (EMA) — announced in October 2021 — is a far more ambitious 7-year, 5-billion-kilometre cruise to seven main-belt asteroids culminating in a 2034 rendezvous and landing on (269) Justitia, targeting a late-2028 launch on a commercial U.S. launcher [3][4]. Both missions are executed by the Mohammed Bin Rashid Space Centre (MBRSC) in collaboration with the Laboratory for Atmospheric and Space Physics (LASP) at the University of Colorado Boulder, anchoring an Emirati deep-space industrial and knowledge-transfer capability [1][3].
Read program brief →ExoMars is ESA's flagship Mars astrobiology programme, anchored by the Rosalind Franklin rover targeting a two-metre subsurface drill — the first instrument ever flown to Mars capable of accessing depths where ancient biosignatures may be preserved from radiation damage [1][2]. Originally a joint ESA-Roscosmos mission, the rover was unwound from Russia in March 2022 in response to the invasion of Ukraine and re-baselined under a Europeanised architecture with a new ESA-built landing platform, NASA contributions, and launch no earlier than 2028 on a commercial U.S. launcher, with arrival at Oxia Planum in 2030 [3][4][5].
Read program brief →NASA's Mars Exploration Program is a multi-decade portfolio of robotic orbiters, landers and rovers — Curiosity (still operational since August 2012), Perseverance (with Ingenuity helicopter, Feb 2021), MAVEN, MRO and Mars Odyssey — plus the embattled $11B+ Mars Sample Return campaign currently under architectural restructure following a 2023 Independent Review Board finding that the planned mission would cost $8-11B and slip to 2040 [1][2][3][4]. The program sustains roughly $600-800M/year in NASA Science Mission Directorate spending and underpins multi-decade contracts at Lockheed Martin (rover descent stages), Aerojet Rocketdyne (RS-25-class propulsion via L3Harris), Maxar (instruments), and JPL/Caltech (integration) [5][6][7].
Read program brief →Tianwen (天问, 'Questions to Heaven') is China's Mars exploration programme — Tianwen-1 (launched July 23, 2020, arrived Mars orbit February 10, 2021) made China the second nation to successfully soft-land and operate a rover (Zhurong) on Mars in May 2021, and the planned Tianwen-3 sample-return mission (NET 2028) targets first return of Mars samples to Earth, potentially ahead of NASA's reformulated Mars Sample Return programme [1][2][3]. Executed by CAST and CALT under CASC, with no listed pure-play exposure and a credible chance of beating NASA / ESA to a Mars sample-return first [4].
Read program brief →The most ambitious planetary science mission ever attempted — bringing Mars rocks to Earth for laboratory analysis.
Sample Cache
24 tubes
Jezero Crater
Target Return
~2035
TBD post-redesign
Cost Estimate
$5.3B–$11B
Lifecycle (2024 review)
Partners
NASA + ESA
Joint campaign
Perseverance has collected and cached 24 titanium sample tubes in Jezero Crater, depositing 10 at the Three Forks depot as backup. Samples include diverse rock types from the ancient river delta.
Following NASA's independent review board (2024) estimating $5.3–11B lifecycle costs, NASA and ESA initiated a programme redesign to identify a lower-cost architecture while preserving scientific return. Multiple concept studies underway.
A NASA-built lander carrying the Mars Ascent Vehicle (MAV) must land near the Three Forks depot, retrieve Perseverance's cached tubes (or collect them via a fetch rover), and launch them into Mars orbit.
The ESA-built Earth Return Orbiter captures the Orbiting Sample container in Mars orbit, stores it safely, and performs a multi-year cruise back to Earth.
A re-entry capsule delivers the sample container to Earth (likely a Utah desert landing). Samples will be distributed to international laboratories for astrobiology and geochemistry analysis.
View full MSR mission entry
Complete mission specs, contractor details, and programme history in our Mars missions comparison hub.
Every major documented Mars dust storm from the Viking era to 2018 — with the missions affected and scientific significance of each event.
| Year | Name | Scale | Duration |
|---|---|---|---|
| 1971 | 1971 Planet-Encircling Dust Storm Effectively opaque from orbit — entire disk featureless in visible light | Global | ~100 days |
| 1977 | 1977 Global Dust Storm A (Viking Era, First Storm) | Global | ~45 days |
| 1977 | 1977 Global Dust Storm B (Viking Era, Second Storm) | Global | ~43 days |
| 2001 | 2001 Planet-Encircling Dust Storm Tau > 5 at multiple locations (near-complete solar opacity at surface) | Global | ~128 days |
| 2007 | 2007 Regional Dust Storm (MER Solar Panel Crisis) Tau ~5.5 at Opportunity's location (solar panel output fell to <1% of normal) | Regional | ~53 days |
| 2018 | 2018 Planet-Encircling Dust Storm Tau > 8.0 at Opportunity's Perseverance Valley location — complete opacity | Global | ~104 days |
| 2019 | 2019 Regional Dust Storm (Post-Global Event) | Regional | ~54 days |
| 2021 | Jezero Crater Dust Devil Activity (Perseverance Era) | Local | Unknown |
Mars dust activity follows a strongly seasonal pattern tied to orbital position (solar longitude Ls) and the eccentricity of Mars's orbit. Because Mars's orbit is significantly more elliptical than Earth's (eccentricity ~0.093), the planet receives ~40% more solar energy at perihelion (Ls 251°) than at aphelion (Ls 71°). This pronounced annual forcing drives a predictable dust season centred on southern summer / perihelion passage. The northern hemisphere spring and summer (Ls 0°–180°) is the quietest dust period. Local and regional storms can initiate at any season but are statistically much more likely from Ls 180° onward.
Peak Risk Season
Ls 180–270
Southern spring and summer, centred on Mars's perihelion at Ls 251°. Enhanced solar heating of the southern hemisphere drives stronger thermal tides and surface winds, greatly increasing the probability of regional and global dust storm initiation. All documented global storms have begun during this window or shortly outside it.
Global Storm Frequency
~1 planet-encircling storm every 3–5 Mars years on average, based on the observational record from 1971 to 2026. Events have occurred in: 1971, 1977 (×2), 1982, 1994 (partial), 2001, 2018. Not every perihelion season produces a global event.
Mission Impact
Solar-powered missions face the greatest risk during perihelion dust season. Power reduction of 50–99% is possible during regional or global storms. Nuclear-powered missions (Curiosity, future missions) are immune to power loss but still experience instrument exposure and reduced visibility. Dust deposition rates and occasional cleaning events (wind gusts) determine long-term solar panel efficiency trends.
2018 Global Storm — Opportunity's Last
The 2018 planet-encircling dust storm initiated in late May 2018, reached global scale by June, and reduced solar panel output on the Opportunity rover to near zero. The solar-powered rover entered emergency hibernation on June 10, 2018 — its last communication. Despite over 1,000 recovery attempts by NASA JPL, Opportunity never woke up. The mission was officially declared over on February 13, 2019, after 14+ years and 45.16 km of surface exploration.
What Mars actually offers for in-situ resource utilization — and what the honest limitations are. Every claim carries a credible counter-argument from primary literature.
Location: Global atmosphere (95.3% CO2 by volume)
MOXIE on Perseverance demonstrated O2 production from CO2 via SOXE (solid oxide electrolyzer) — 6g/hour at scale needed for launch propellant means scaling to 25 kg/day for MAV
Skeptic's view
Atmospheric density is only 0.6% of Earth's — thin enough that large collectors are needed; power requirements are substantial
Location: Equatorial and low-latitude zones — usable globally but reduced by ~40-45% vs Earth
Primary power source for landed assets without RTGs — Perseverance uses RTG while Ingenuity uses solar panels as test case; future crewed habitats must use nuclear fission (Kilopower/KRUSTY) or large solar arrays
View resource details →Location: Global — regolith covers entire Martian surface
Structural material for 3D-printed habitats (analogous to terrestrial sintered bricks), iron extraction for manufacturing, thermal mass for passive heating
View resource details →Location: Mid-latitudes (30°–60° N and S), within 1–5 meters of surface
Primary water source for crewed surface habitats; mining with heated drill could extract several liters/hour per site
View resource details →Location: North and South Poles; north cap is water ice year-round, south cap CO2 ice over water ice
Electrolysis to produce rocket propellant (H₂+O₂), life support water and oxygen for crewed missions, radiation shielding via water walls
Skeptic's view
Polar ice is far from equatorial landing sites — nearest useful water ice deposits are mid-latitude subsurface glaciers
Location: Widespread — Noachian basalts (ancient), Amazonian volcanic plains
Silica for glass production, olivine/pyroxene for geopolymer cement without heating, basalt fiber composite materials for structural applications
View resource details →Location: Global — detected at Phoenix landing site (68°N), Gale Crater (Curiosity), Jezero Crater (Perseverance)
Ammonium perchlorate is a solid rocket oxidizer — in theory Martian perchlorates could be chemically processed into propellant components; also possible source of oxygen via thermal decomposition
Skeptic's view
Perchlorates are highly toxic to humans and other organisms — a major challenge for habitability and agriculture. Must be removed from any soil used for growing food
Location: Volcanic regions: Tharsis Bulge, Elysium Planitia — areas of potential residual geological heat
If accessible — geothermal could power crewed outposts without nuclear or solar dependence
Skeptic's view
InSight detected very low heat flux (~21 mW/m² near Elysium Planitia) — far below economically viable geothermal extraction; Mars may be too geologically cold for practical geothermal
Short, sourced answers to the most common questions about Mars exploration, habitability, and the path to crewed missions.