{{Short description|Cancelled mission to remove space debris}} {{lowercase title}} {{Use dmy dates|date=June 2015}} {{Infobox spaceflight | name = e.Deorbit | names_list = <!--image of the spacecraft/mission--> | image = <!--omit the "file" prefix--> | image_caption = <!--image caption--> | image_alt = <!--image alt text--> | image_size = <!--include px/em; defaults to 220px-->
<!--Basic details--> | mission_type = Active debris removal | operator = ESA | Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)--> | COSPAR_ID = <!--spacecraft launched since 1963 only (aka NSSDC ID; eg. 1998-067A)--> | SATCAT = <!--satellite catalogue number, omit leading zeroes (e.g. 25544)--> | website = <!--Homepage of the craft/mission, OFFICIAL PAGES ONLY--> | mission_duration = <!--How long the mission lasted--> | distance_travelled = <!--How far the spacecraft travelled (if known)--> | orbits_completed = <!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit--> | suborbital_range = <!--downrange distance reached if spacecraft did not enter orbit--> | suborbital_apogee = <!--altitude reached if spacecraft did not enter orbit-->
<!--Spacecraft properties--> | spacecraft = <!--Spacecraft name/serial number (eg. Space Shuttle ''Discovery'', Apollo CM-118), etc--> | spacecraft_type = <!--eg. GPS Block II, Kobalt-M, US-K, etc--> | spacecraft_bus = <!--eg. A2100M, Star-2, etc--> | manufacturer = <!--company or companies who built the satellite--> | launch_mass = {{convert|1600|kg}} | BOL_mass = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase--> | landing_mass = <!--Mass after landing (recovered spacecraft only)--> | dry_mass = <!--spacecraft mass in orbit without fuel--> | payload_mass = <!--Mass of cargo carried by spacecraft (eg. for Space Shuttle), or total mass of instrumentation/equipment/experiments for mission--> | dimensions = <!--body dimensions and solar array span--> | power = <!--end-of-life power, in watts-->
<!--Launch details--> | launch_date = 2025 (planned)<ref name="NewMission" /> | launch_rocket = Vega | launch_site = ELA-1, Guiana Space Centre | launch_contractor = Arianespace | deployment_from = <!--place where deployed from--> | deployment_date = <!--date deployed--> | entered_service = <!--date on which the spacecraft entered service, if it did not do so immediately after launch--> <!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur-->
<!--end of mission--> | disposal_type = Deorbit (planned) | deactivated = <!--when craft was decommissioned--> | destroyed = <!--when craft was destroyed (if other than by re-entry)--> | last_contact = <!--when last signal received if not decommissioned--> | recovery_by = <!--recovered by--> | recovery_date = <!--recovery date--> | decay_date = <!--when craft re-entered the atmosphere, not needed if it landed--> | landing_date = <!--when the spacecraft made a controlled landing, not needed if it did not return intact--> | landing_site = <!--where the craft landed; site/runway or coordinates--> <!-- The following template should be used for ONE of the three above fields "end_of_mission", "decay" or "landing" if the spacecraft is no longer operational. If it landed intact, use it for the landing time, otherwise for the date it ceased operations, or the decay date if it was still operational when it re-entered. {{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown) -->
<!--orbit parameters--> <!--as science-related articles, SI units should be the principal units of measurement, however we usually use {{convert}} to display imperial units in parentheses after the initial values--> | orbit_reference = <!--geocentric, selenocentric, etc - please link (e.g. Geocentric)--> | orbit_regime = <!--high, low, medium, molniya, GSO - please link (e.g. Low Earth - please don't use acronyms--> | orbit_longitude = <!--geosynchronous satellites only--> | orbit_slot = <!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)--> | orbit_semimajor = <!--semimajor axis--> | orbit_eccentricity = <!--orbital eccentricity--> | orbit_periapsis = <!--periapsis altitude--> | orbit_apoapsis = <!--apoapsis altitude--> | orbit_inclination = <!--orbital inclination--> | orbit_period = <!--time taken to complete an orbit--> | orbit_RAAN = <!--right ascension of the ascending node--> | orbit_arg_periapsis = <!--argument of perigee/periapsis--> | orbit_mean_anomaly = <!--mean anomaly at epoch, only use in conjunction with an epoch value--> | orbit_mean_motion = <!--mean motion of the satellite, usually measured in orbits per day--> | orbit_repeat = <!--repeat interval/revisit time--> | orbit_velocity = <!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity--> | orbit_epoch = <!--the date at which the orbit parameters were correct--> | orbit_rev_number = <!--revolution number--> | apsis = <!--planet specific apsis term (eg. gee/helion/selene/etc - defaults to generic "apsis")-->
| docking = <!--Infobox spaceflight/Dock can be called multiple times for missions with multiple dockings--> {{Infobox spaceflight/Dock | docking_target = derelict satellite <!--spacecraft docked with--> | docking_type = capture <!--delete as appropriate--> | type_override = berth <!--delete if docking_type is not set to "capture"--> | docking_port = <!--port at which the spacecraft docks/berths, if the target has more than one--> | docking_date = <!--date/time of docking/berthing--> | undocking_date = <!--date/time of undocking/unberthing--> | capture_date = <!--RMS capture for berthed craft--> | release_date = <!--RMS release for berthed craft--> | time_docked = <!--time the spacecraft spent docked--> }}
<!--Cargo parameters--> | payload_items = <!--Major individual items (e.g. satellites deployed, etc)--> | cargo_mass = <!--Mass of the cargo aboard--> | cargo_mass_press = <!--Mass of pressurised cargo--> | cargo_mass_unpress = <!--Mass of unpressurised cargo (e.g. Dragon Trunk)--> | cargo_mass_fuel = <!--Mass of fuel transferred from spacecraft's tanks--> | cargo_mass_gas = <!--Mass of gasses transferred (e.g. oxygen)--> | cargo_mass_water = <!--Mass of water transferred-->
<!--transponder parameters--> | trans_band = <!--Transponder frequency bands--> | trans_frequency = <!--specific frequencies--> | trans_bandwidth = <!--bandwidth--> | trans_capacity = <!--capacity of the transponders--> | trans_coverage = <!--area covered--> | trans_TWTA = <!--TWTA output power--> | trans_EIRP = <!--equivalent isotropic power--> | trans_HPBW = <!--half-power beam width-->
<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions. If in doubt, leave it out--> | programme = | previous_mission = | next_mission =
<!--mission insignia or patch--> | insignia = <!--omit the "file" prefix--> | insignia_caption = <!--image caption--> | insignia_alt = <!--image alt text--> | insignia_size = <!--include px/em; defaults to 180px--> }} '''e.Deorbit ''' was a planned European Space Agency active space debris removal mission developed as a part of their Clean Space initiative.<ref name="ESAconference1">{{cite web|url=https://indico.esa.int/indico/event/46/|title=e.Deorbit Symposium|publisher=ESA|date=6 May 2014|access-date=2 June 2015|archive-date=1 July 2015|archive-url=https://web.archive.org/web/20150701150318/https://indico.esa.int/indico/event/46/|url-status=dead}}</ref><ref name="GizmagFishing">{{cite web|url=http://www.gizmag.com/esa-clean-space-junk-edeorbit/30972/|title=Space fishing: ESA floats plan to net space junk|publisher=Gizmag|date=28 February 2014|access-date=2 June 2015}}</ref> The launch was planned for 2025 on board a Vega launch vehicle.<ref name="NewMission">{{cite web |last=Pultarova |first=Tereza |url=https://www.space.com/43157-e-deorbit-new-refuel-repair-mission.html |title=European Space Junk Cleanup Concept Gets New Mission: Refuel and Repair |work=Space.com |date=29 January 2019 |access-date=16 October 2019}}</ref><ref name="e.Deorbit">{{cite news|url=https://www.esa.int/Our_Activities/Space_Engineering_Technology/Clean_Space/e.Deorbit/|title=E.DEORBIT Mission|publisher=ESA|date=12 April 2017|access-date=6 October 2018}}</ref><ref name="ESAheading">{{cite news|url=https://www.esa.int/Our_Activities/Space_Engineering_Technology/Clean_Space/ESA_heading_towards_removing_space_debris|title=ESA heading towards removing space debris|publisher=ESA|date=2 June 2015|access-date=2 June 2015}}</ref> Funding of the mission was stopped in 2018<ref>{{cite web|url=https://blogs.esa.int/cleanspace/2018/11/26/from-active-debris-removal-to-in-orbit-servicing-the-legacy-of-e-deorbit/|title=From Active Debris Removal To In-Orbit Servicing: THE LEGACY OF e.Deorbit|date=26 November 2018}}</ref> in favor of the ClearSpace-1 mission, which is now under development.<ref name="esa.int">[https://www.esa.int/Safety_Security/Clean_Space/ESA_commissions_world_s_first_space_debris_removal ESA commissions world’s first space debris removal]</ref>
==Overview== A {{convert|1600|kg|adj=on}} spacecraft was to be launched on board a Vega rocket into a polar orbit at an altitude of {{convert|800-1000|km|mi}}. Once on orbit, the spacecraft would rendezvous with the derelict satellite Envisat which is in an unknown condition, inoperative, and probably tumbling.<ref name="GizmagFishing" />
Capture would be conducted in one of two ways: either by using mechanical tentacles or nets. The tentacles option included equipping the spacecraft with robotic arms, one of which will first capture a holding point, before the remaining arms embrace the derelict and secure it with a clamping mechanism. The net option included equipping the spacecraft with a deployable net on a tether, that will envelop the target derelict before the spacecraft will begin changing orbit.<ref name="CDFstudy2013">{{cite web|url=http://iaassconference2013.space-safety.org/wp-content/uploads/sites/19/2013/06/1200_Biesbroek_Innocenti.pdf|title=The e.Deorbit CDF Study|author=Robin Biesbroek|date=22 May 2013|access-date=2 June 2015}}</ref>{{Reference page|pages=13,24–25}} The net option has the advantage of being able to capture objects with a wide range of sizes and spins.<ref name="VOnets">{{cite web|url=http://blogs.voanews.com/science-world/2015/03/23/fishing-in-outer-space-for-bigger-junk/|archive-url=https://web.archive.org/web/20150327000557/http://blogs.voanews.com/science-world/2015/03/23/fishing-in-outer-space-for-bigger-junk/?|url-status=dead|archive-date=27 March 2015|title=Fishing in Outer Space for Bigger Junk|publisher=Voice of America|author=Rick Pantaleo|date=23 March 2015|access-date=2 June 2015}}</ref>
After successfully capturing the targeted derelict, the spacecraft would deorbit itself, performing a controlled atmospheric reentry.<ref name="ESAheading"/>
==History== The mission was developed at ESA's Concurrent Design Facility, with studies for the Clean Space programme on de-orbiting techniques being carried out in 2009.<ref name="ESAheading" /><ref name="CDFcleanSpace">{{cite web|url=http://www.esa.int/Our_Activities/Space_Engineering_Technology/CDF/Clean_Space|title=Clean Space|publisher=ESA, Concurrent Design Facility|date=3 October 2012|access-date=2 June 2015}}</ref> The first symposium about the mission took place in May 2014.<ref name="ESAconference1"/> Early testing included successful attempts at capturing scale model satellites by shooting nets from compressed air ejectors.<ref name="VOnets" /> The first design stage was completed in June 2015, with a systems requirements review being conducted in May–June 2016 and a final mission approval taking place in December 2016.<ref name="ESAheading" />
==See also== *RemoveDEBRIS, a similar concept that combined four experiments for future Active Debris Removal technology: a net, a harpoon, a Vision-Based Navigation (VBN) system and a dragsail.<ref>"The active space debris removal mission RemoveDebris". Parts 1 and 2 (https://doi.org/10.1016/j.actaastro.2019.09.002, https://doi.org/10.1016/j.actaastro.2019.09.001)</ref> *ClearSpace-1, the follow-up of e.Deorbit: a mission that will use e.Deorbit's tentacles option to capture the PROBA-1 satellite.
==References== {{reflist}}
==External links== * [http://www.esa.int/Our_Activities/Space_Engineering_Technology/Clean_Space ESA Clean Space] website * [http://www.esa.int/spaceinimages/Images/2013/09/Space_debris_removal_mission Space debris removal mission] ESA illustration * [http://www.esa.int/Our_Activities/Space_Engineering_Technology/Clean_Space/Readying_ESA_s_garbage_truck_Robin_Biesbroek_interview Interview with Robin Biesbroek], e.Deorbit study manager
{{European Space Agency}}
Category:Space debris Category:Proposed European Space Agency spacecraft