|Names||Phobos Sample Return Mission|
|Mission type||Technology demonstrattor, sample return|
|Operator||European Space Agency|
|Mission duration||3.5 years (planned)|
|Manufacturer||Airbus Defense and Space|
|Launch mass||4,200 kg (9,300 lb)|
|Start of mission|
|Launch date||2024 (proposed)|
|Launch site||Guiana Space Centre|
|End of mission|
|Sample mass||800 g; return about 100 g (0.22 lb)|
Overview and status
The Phootprint mission is a candidate for the Mars Robotic Exploration Preparation Programme 2 (MREP-2) at ESA. During 2014, ESA funded a pre-phase A feasibility study and industrial system studies of 8-month duration. Currently, it is in phase A, meaning 'mission definition study.'
The mission is proposed to be launched with an Ariane 5 on 2024 with early 2026 as backup date. An Earth swingby would provide greater launcher margin. The spacecraft would orbit Mars for the characterisation phase, and when ready, it would maneuver into a quasi-satellite orbit to facilitate landing. Because of the low gravity, the lander would be anchored to the surface during sample collection and launch of the Earth Re-entry Capsule (ERC).
The top-level science goal is to understand the formation of the Martian moons Phobos and Deimos and put constraints on the evolution of the Solar System (co-formation, capture, impact ejecta).
The mission objectives are: 
- Return 100 g of loose material from the surface of Phobos.
- Access at least 50% of the Phobos surface for the sampling operations.
- Landing site selected by Science Team during mission post extensive global and local mapping campaign
- Strict requirements on surface contamination
- Goal of 800 g load on sample (return approximately 100 g (0.22 lb))
- Static landing with 100 m (330 ft) landing accuracy
Mission engineers remark that "no rebound" after landing is a critical condition given the low-gravity environment of landing. Currently, engineers at ESA are leaning toward four cantilever-type landing legs with crushable aluminium honeycomb shock absorber and secondary load limiters.
The preliminary concept of Phootprint spacecraft is still preliminary and composed by three modules: 
- The Landing Module (LM) carrying the ERV & ERC, performing the transfer to Mars, the Mars orbit insertion and phasing manoeuvres to reach Phobos vicinity, the operations around and on Phobos, including landing and sampling. The landing Module would be equipped with a 2 m (6 ft 7 in) sampling robotic arm.
- The Earth Return Vehicle (ERV) performing the Mars escape, the transfer back to Earth and the ERC release few hours before re-entry.
- The Earth Re-entry Capsule (ERC) — fully passive concept: ballistic re-entry, no parachute, hard landing on ground with maximum impact deceleration of 1700 g to the sample. Modeling of the thermal design indicates the sample container temperature during reentry would be less than 40 °C (104 °F). A location beacon would be included within sample container.
As of 2014, a 30 kg payload is foreseen: 
- Wide Angle Camera
- Narrow Angle Camera
- Close-Up Camera
- Context camera for sampling context
- Visible-IR spectrometer
- Infrared spectrometer
- and a Radio Science investigation
The proposed mission architecture is: 
- Ariane 5 launch from Kourou in direct escape
- Transfer to Mars (11 months)
- Nine months orbiting Phobos/Mars dedicated to science observations and sampling (7 days on the surface)
- Departure from Mars to Earth (8 months)
- Fobos Grunt
- Missions to the moons of Mars
- Phobos And Deimos & Mars Environment (PADME)
- Phobos program
- Phobos Surveyor
- Barraclough, Simon; Ratcliffe, Andrew; Buchwald, Robert; Scheer, Heloise; Chapuy, Marc; Garland, Martin (June 16, 2014). Phootprint: A European Phobos Sample Return Mission (PDF). 11th International Planetary Probe Workshop. Airbus Defense and Space.<templatestyles src="Module:Citation/CS1/styles.css"></templatestyles>
- Supporting the Mars Robotic Exploration Preparation Programme. ESA. 4 July 2015.
- Koschny, Detlef; Svedhem, Håkan; Rebuffat, Denis (August 2, 2014). "Phootprint - A Phobos sample return mission study". ESA. Retrieved 2015-12-22.<templatestyles src="Module:Citation/CS1/styles.css"></templatestyles>
- "ESA at MAKS 2015". European Space Agency. Zhukovsky, Russia: ESA. Retrieved 2015-12-22.<templatestyles src="Module:Citation/CS1/styles.css"></templatestyles>
- Kane, Van (9 June 2014). "A Checkup on Future Mars Missions". The Planetary Society. Retrieved 2015-12-22.<templatestyles src="Module:Citation/CS1/styles.css"></templatestyles>
- Chitu, Cristian Corneliu; Stefanescu, Raluca; Bajanaru, Paul; Galipienzo, Julio; Rybus, Tomasz; Seweryn, Karol; Visentin, Gianfranco; Ortega, Cristina; Barciński, Tomasz (2014). Design and Development of an Active Landing Gear System for Robotically Enhanced Surface Touchdown (PDF). European Space Research and Technology Centre. European Space Agency.<templatestyles src="Module:Citation/CS1/styles.css"></templatestyles>
-  "Sample Return Missions Requirements for Earth Reentry Capsules TPS". D. Rebuffat. ESA.