Phootprint

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Phootprint
Names Phobos Sample Return Mission
Mission type Technology demonstrattor, sample return
Operator European Space Agency
Mission duration 3.5 years (planned)[1]
Spacecraft properties
Manufacturer Airbus Defense and Space
Launch mass 4,200 kg (9,300 lb)[1]
Start of mission
Launch date 2024 (proposed)
Rocket Ariane 5
Launch site Guiana Space Centre
End of mission
Disposal Re-entry capsule
Landing date ~2027
Orbital parameters
Reference system Mars
Phobos
Phobos lander
Sample mass 800 g; return about 100 g (0.22 lb)

Phootprint is a proposed sample-return mission to the Mars moon Phobos by the European Space Agency (ESA), proposed to be launched in 2024.

Overview and status

The Phootprint mission is a candidate for the Mars Robotic Exploration Preparation Programme 2 (MREP-2) at ESA.[1] During 2014, ESA funded a pre-phase A feasibility study and industrial system studies of 8-month duration.[1][2] Currently, it is in phase A, meaning 'mission definition study.'

The mission is proposed to be launched on an Ariane 5 in 2024 with early 2026 as backup date.[1] An Earth swingby would provide greater launcher margin.[1] The spacecraft would orbit Mars for the characterisation phase,[1][3] and when ready, it would maneuver into a quasi-satellite orbit to facilitate landing.[1] 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 mission would last about 3.5 years, including cruise, mapping orbit, 7 days on the surface, and sample return cruise time.[1] The spacecraft would be powered by solar arrays.

In August 2015, the ESA-Roscosmos working group on post-ExoMars cooperation, completed a joint study for a possible future Phobos Sample Return mission, and preliminary discussions were held.[4][5]

Objectives

Phobos, one of the two moons of Mars
Parent body, the planet Mars

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).[1]

The mission objectives are:[1]

  • Return 100 grams (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.[6] Currently, engineers at ESA are leaning toward four cantilever-type landing legs with crushable aluminium honeycomb shock absorber and secondary load limiters.[1]

Spacecraft

The concept of the Phootprint spacecraft is still preliminary and composed by three modules:[6]

  • 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.[1] 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.

Proposed payload

As of 2014, the conceptual 30 kg (66.1 lb) payload is:[3]

  • Wide angle camera
  • Narrow angle camera
  • Close-up camera
  • Context camera for sampling context
  • Visible-IR spectrometer
  • Infrared spectrometer
  • a radio science investigation

Mission architecture

The proposed mission architecture is:[7]

  1. Ariane 5 launch from Kourou in direct escape
  2. Transfer to Mars (11 months)
  3. Nine months orbiting Phobos/Mars dedicated to science observations and sampling (7 days on the surface)
  4. Departure from Mars to Earth (8 months)

See also

References

  1. ^ a b c d e f g h i j k l m 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.
  2. ^ Supporting the Mars Robotic Exploration Preparation Programme. ESA. 4 July 2015.
  3. ^ a b Koschny, Detlef; Svedhem, Håkan; Rebuffat, Denis (August 2, 2014). "Phootprint - A Phobos sample return mission study". ESA. Bibcode:2014cosp...40E1592K. Missing or empty |url= (help); |access-date= requires |url= (help)
  4. ^ "ESA at MAKS 2015". European Space Agency. Zhukovsky, Russia: ESA. Retrieved 2015-12-22.
  5. ^ Kane, Van (9 June 2014). "A Checkup on Future Mars Missions". The Planetary Society. Retrieved 2015-12-22.
  6. ^ a b 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.
  7. ^ [1] "Sample Return Missions Requirements for Earth Reentry Capsules TPS". D. Rebuffat. ESA.
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