Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Phootprint

From Wikipedia, the free encyclopedia

Proposed sample-return mission to Phobos
Phootprint
NamesPhobos Sample Return Mission
Mission typeTechnology demonstrattor, sample return
OperatorEuropean Space Agency
Mission duration3.5 years (planned)[1]
Spacecraft properties
ManufacturerAirbus Defence and Space
Launch mass4,200 kg (9,300 lb)[1]
Start of mission
Launch date2024 (proposed)
RocketAriane 5
Launch siteGuiana Space Centre
End of mission
DisposalRe-entry capsule
Landing date~2027
Orbital parameters
Reference systemMars
Phobos
Phobos lander
Sample mass800 g; return about 100 g (0.22 lb)

Phootprint was a feasibility study conducted in 2014 by theEuropean Space Agency (ESA) for a sample-return mission to theMars moonPhobos. The study proposed a launch date of 2024 for this mission.[1] The ESA ultimately did not launch Phootprint as its own mission but is working with the Japan Aerospace Exploration Agency (JAXA) on theMartian Moons eXploration (MMX) probe, a similar mission to Phobos set to launch in 2026.[2]

Overview and status

[edit]

The Phootprint mission was conceived as a candidate for the Mars Robotic Exploration Preparation Programme 2 (MREP-2) at ESA.[1] In 2014, ESA funded Footprint's pre-phase A feasibility study and an 8-month industrial system study.[1][3]

The mission was proposed to be launched on anAriane 5 in 2024 with early 2026 as backup date.[1] The spacecraft would have orbited Mars for the characterisation phase,[1][4] before maneuvering into a quasi-satellite orbit to facilitate the landing on Phobos.[1] Because of the low gravity, the lander would have anchored itself to the surface during sample collection and when launching the Earth Re-entry Capsule (ERC).

The mission would have lasted about 3.5 years, including the cruise time to Phobos, orbit mapping, 7 days on the surface, and finally, the sample return cruise time.[1] The spacecraft would be powered bysolar arrays.

In August 2015, theESA-Roscosmos working group, after cooperation onExoMars, completed a joint study for a possible future Phobos Sample Return mission, and preliminary discussions were held.[5][6]

Ultimately, Phootprint was not pursued as an ESA-headed mission under that name. However, interest in a sample-return mission to Phobos remained to further the objectives of the ESA'sCosmic Vision campaign, and the ESA became a contributor to the JapaneseMMX mission.[2]

Objectives

[edit]
Phobos, one of the two moons of Mars
Parent body, the planet Mars

The top-level science goal was 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 were:[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

"No rebound" after landing was a critical condition given the low-gravity environment of Phobos.[7] To address this, the feasibility study recommended fourcantilever-type landing legs with crushable aluminumhoneycombshock absorbers and secondary load limiters.[1]

Spacecraft

[edit]

The concept of the Phootprint spacecraft was composed of three modules:[7]

  • The Landing Module (LM) carrying the ERV & ERC, performing the transfer to Mars, the Mars orbit insertion and phasing maneuvers 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 a few hours before re-entry.
  • The Earth Re-entry Capsule (ERC) — a fully passive module: ballistic re-entry with no parachute, hard landing on the 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

[edit]

The conceptual 30 kg (66.1 lb) payload was:[4]

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

Mission architecture

[edit]

The proposed mission architecture was:[8]

  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

[edit]

References

[edit]
  1. ^abcdefghijklmBarraclough, 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.Archived(PDF) from the original on January 29, 2016. RetrievedDecember 22, 2015.
  2. ^ab"MMX factsheet".www.esa.int.Archived from the original on 9 June 2025. Retrieved6 November 2025.
  3. ^Supporting the Mars Robotic Exploration Preparation Programme.ESA. 4 July 2015.
  4. ^abKoschny, Detlef; Svedhem, Håkan; Rebuffat, Denis (August 2, 2014). "Phootprint - A Phobos sample return mission study".ESA.40: B0.4–9–14.Bibcode:2014cosp...40E1592K.
  5. ^"ESA at MAKS 2015".European Space Agency. Zhukovsky, Russia: ESA. Retrieved2015-12-22.
  6. ^Kane, Van (9 June 2014)."A Checkup on Future Mars Missions".The Planetary Society. Retrieved2015-12-22.
  7. ^abChitu, 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.
  8. ^[1]Archived 2015-11-17 at theWayback Machine "Sample Return Missions Requirementsfor Earth Reentry Capsules TPS". D. Rebuffat. ESA.
Space Centres
Launch vehicles
Facilities
Communications
Programmes
Predecessors
Related topics
Science
Astronomy
& cosmology
Earth
observation
Planetary
science
Solar
physics
Human
spaceflight
Telecommunications
and navigation
Technology
demonstration
and education
Launch
and reentry
Proposed
Cancelled
Failed
Future missions initalics
Active
Flybys
Orbiters
Rovers


Past
Flybys
Orbiters
Landers
Rovers
Aircraft
Failed
launches
Future
Planned
Proposed
Cancelled
or not developed
Exploration
Concepts
Strategies
Advocacy
Missions are ordered by launch date. Sign indicates failure en route or before intended mission data returned. indicates use of the planet as agravity assist en route to another destination.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Phootprint&oldid=1320783328"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp