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IXV is the second large spacecraft which ESA has attempted to recover from space, and builds on the Advanced Reentry Demonstrator (ARD) mission, launched on the third flight of the Ariane 5 in October 1998.<\/p>\n
ARD was a conical capsule which was retrieved from the Pacific following a 101-minute mission.<\/p>\n
Like IXV, this was an experimental mission; ESA has never operated a reusable spacecraft operationally, instead relying on Russian and American spacecraft to carry scientific and technological experiments requiring a return to Earth.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_48_45-LIVE_-Vega-flight-VV04-IXV-February-11-2015-13_00-UTC-350x245.jpg\")
Measuring five metres in length, 2.2 metres in width and 1.5 metres in height (16.4 by 7.2 by 4.9 ft), the IXV has a mass of 1,845 kilograms (4,068 lb).<\/p>\nIt was constructed for ESA by Italian aerospace company NGL Prime. Jointly owned by Airbus and Finmeccanica, NGL, which stands for Next Generation Launcher, is the prime contractor for ESA\u2019s Future Launchers Preparatory Programme (FLPP), a programme which the agency is undertaking to improve its current-generation rockets and lead into the development of a new generation of vehicles.<\/p>\n
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While there are no serious plans at present for any of these rockets to be recoverable, the IXV will provide data for the programme and could lead to advances in European spacecraft technology.<\/p>\n
![\"\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/02\/Z69.jpg\")
Arianespace launched the IXV using a Vega rocket.<\/p>\nMaking its fourth flight, the Vega is a four-stage vehicle designed to carry small satellites into low Earth orbit.<\/p>\n
First flown in February 2012, the Vega is the smallest of the three rockets in Arianespace\u2019s fleet, along with the Russian-built Soyuz-ST and the larger Ariane 5.<\/p>\n
On its first launch, Vega carried the LARES geodesy research satellite and a collection of CubeSats into orbit, while subsequent launches in May 2013 and April 2014 carried ESA\u2019s experimental PROBA-V Earth observation satellite and Kazakhstan\u2019s KazEOSat-1 imaging spacecraft.<\/p>\n
All of the rocket\u2019s flights to date have been successful.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_50_45-Vega-Pad-ESA-Google-Search-350x248.jpg\")
Wednesday\u2019s launch, designated VV04, took place from the Vega\u2019s launch pad at the Centre Spatial Guyanais, or Guiana Space Centre, in Kourou, French Guiana.<\/p>\nVariously designated Zone de lancement Vega (ZLV), Ensemble de lancement Vega (ELV) and Site de lancement Vega (SLV), the pad was originally built in the early 1970s for the European Launcher Development Organisation (ELDO).<\/p>\n
A single Europa II vehicle was flown from Guiana by ELDO, failing to achieve orbit with a vehicle evaluation payload. This proved the final launch of the Europa rocket, however in 1979 its successor, the Ariane 1, made its maiden flight from the same complex.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_51_51-Vega-Pad-ESA-Google-Search-350x252.jpg\")
The pad, designated Ensemble de lancement Ariane (ELA) and later ELA-1 after a new pad was constructed for the Ariane 4, supported 25 Ariane launches between 1979 and 1989, ending with the final flight of the Ariane 3.<\/p>\nWith the larger Ariane 4 and later 5 rockets flying from ELA-2 and ELA-3 respectively, ELA-1 fell into disuse and was decommissioned. Rebuilt for Vega in the late 2000s, the complex now serves as that rocket\u2019s only launch site.<\/p>\n
Launch day activities on Wednesday began eight hours and fifteen minutes before the scheduled launch, at which point controllers began to activate, test and configure the IXV\u2019s ground stations. Arianespace began the seven and three-quarter hour launch countdown at 02:30 local time (05:30 UTC).<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_54_10-ESAs-IXV-reentry-vehicle-mission-YouTube-350x228.jpg\")
About seven and a half hours before liftoff ESA conducted a series of communications tests between the IXV, its ground stations and mission control.<\/p>\nA full test of the spacecraft\u2019s ground segment took place an hour later followed by a voice communications check at the six-hour, fifteen-minute mark.<\/p>\n
Vega\u2019s Multi-Function Unit (MFU), responsible for control over the vehicle\u2019s critical systems including power distribution, pyrotechnics and valve control, was activated five hours and forty minutes ahead of liftoff, followed ten minutes later by the rocket\u2019s inertial guidance system and telemetry transmitters.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_54_41-Vega-Pad-ESA-mission-Google-Search-350x265.jpg\")
At the four-hour, fifty five minute mark in the countdown the rocket\u2019s computers was powered up and the flight plan was loaded into them.<\/p>\nThe rocket\u2019s flight termination system, or Safeguard Master Unit (SMU) in ESA parlance, was powered up at the four hour, fifty minute mark in proceedings.<\/p>\n
While these events are taking place, the IXV team conducted a final mission simulation, concluding four hours and forty five minutes before liftoff.<\/p>\n
The IXV\u2019s own countdown operations began with three and a half hours to go until liftoff.<\/p>\n
At the four hour, twenty five minute mark in the countdown the rocket\u2019s clocks was synchronised to UTC, with alignment and checkout of the guidance system took place five minutes later.<\/p>\n
(L2 Link to 15 Presentations on IXV)<\/p>\n
Preparations for retracting the mobile service tower from around the rocket began at the three hour and forty minute mark with engineers clearing the final remove-before-flight safing devices from the rocket.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_55_39-Fully_assembled_Vega_VV01_on_pad_large.jpg-625%C3%97279-350x264.jpg\")
First motion of the gantry itself began an hour later, with the retraction process taking three quarters of an hour.<\/p>\nEighty minutes before launch the rocket\u2019s remaining telemetry systems and transponders were activated.<\/p>\n
The spacecraft\u2019s ground stations and support segment were placed into launch configuration at the sixty minute point in the countdown, with the rocket reaching launch readiness thirty-four minutes ahead of its planned liftoff.<\/p>\n
Following a final weather report at the ten minute mark in the count, the rocket entered its automated terminal count, or \u201csynchronised sequence\u201d for the last four minutes of the countdown. A delay deep into the window occurred due to a telemetry issue.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_56_38-Vega-Launch-Google-Search-350x240.jpg\")
Once the count reached zero, the P80FW motor which powers the first stage ignited and Vega will begin her ascent.<\/p>\nFlying East the rocket headed out over the Atlantic Ocean, with the first stage burning for one minute and fifty seconds before separation and ignition of the second stage two seconds later.<\/p>\n
A Zefiro-23, this stage powered the vehicle for 77 seconds.<\/p>\n
A further twenty six seconds after burnout, the spent stage separated and the Zefiro-9A third stage ignited to begin its 119-second burn.<\/p>\n
*Click here for IXV News Articles*<\/p>\n
Twenty seven seconds into third stage flight, at an altitude of 117 kilometres (72.7 miles, 63.2 nautical miles), the payload fairing separated from around the IXV.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_57_30-ESAs-IXV-reentry-vehicle-mission-YouTube-350x223.jpg\")
The first three stages of the rocket are all solid-fuelled, burning hydroxyl-terminated polybutadiene (HTPB) 1912 propellant. Vega\u2019s fourth stage, and the only one to use liquid propellant, is the Attitude and Vernier Upper Module, or AVUM.<\/p>\nDesigned to improve the precision of Vega\u2019s orbital insertion by providing fine control during the final stages of launch, the AVUM is powered by a Ukrainian-built RD-869 engine burning unsymmetrical dimethylhydrazine oxidised by dinitrogen tetroxide.<\/p>\n
The stage is tasked with three burns during Wednesday\u2019s mission; the first to establish the IXV on its planned trajectory while the second and third will occur after spacecraft separation as tests of the stage.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_58_31-ESAs-IXV-reentry-vehicle-mission-YouTube-350x243.jpg\")
Following the jettison of the spent third stage, six minutes and 37 seconds after liftoff, the Vega coasted until ignition of the AVUM at eight minutes mission elapsed time.<\/p>\nThe first burn lasted five minutes and forty nine seconds, establishing the desired separation trajectory for the IXV mission.<\/p>\n
Spacecraft separation occurred after around four minutes and ten seconds after the conclusion of the burn; 17 minutes and 59 seconds after liftoff.<\/p>\n
The AVUM\u2019s second burn will last sixteen seconds, beginning 31 minutes and 14 seconds into the flight, while its final 59-second burn will ignite 109 minutes and 31 seconds after liftoff.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_46_56-LIVE_-Vega-flight-VV04-IXV-February-11-2015-13_00-UTC-350x268.jpg\")
The target trajectory for separation of the Intermediate Experimental Vehicle was a perigee of 76 kilometres (47.2 miles, 41.0 nautical miles) and an apogee of 416 kilometres (258 miles, 225 nautical miles) at an inclination of 5.4 degrees.<\/p>\nWhile this could technically be termed an orbit, since the perigee of the trajectory lies above the surface of the Earth, it intersects the atmosphere such that the IXV will reenter before completing its first revolution.<\/p>\n
Such a transatmospheric orbit is generally considered to be a suborbital, rather than orbital, mission.<\/p>\n
Shortly after separation, a tracking station in Libreville, Gabon, acquired the spacecraft\u2019s signal. About three and a half minutes into free flight the spacecraft\u2019s reaction control system were primed to provide attitude control during the mission.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-03_59_28-ESAs-IXV-reentry-vehicle-mission-YouTube-350x232.jpg\")
Handover of the spacecraft\u2019s tracking from Libreville to Malindi, Kenya took place between 23 and 25 and a half minutes after liftoff, with Malindi providing tracking until the expected loss of signal around 34 minutes and 12 seconds mission elapsed time.<\/p>\nThe IXV ascended to its apogee before descending towards reentry. The spacecraft was not expected to be heard from again until after it has reentered the atmosphere, with a tracking ship picking up its signal at one hour and 22 minutes into the flight.<\/p>\n
Three minutes after the acquisition of signal the spacecraft ejected the panel covering its parachute bay and deploy a pilot parachute followed by the first of two drogue chutes.<\/p>\n
![\"2015-02-11](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/02\/2015-02-11-04_00_15-ESAs-IXV-reentry-vehicle-mission-YouTube-350x235.jpg\")
Designed to slow the spacecraft from supersonic speed, this first drogue separated, pulling out a subsonic drogue chute which continued to slow the vehicle.<\/p>\nFour minutes after the panel separated, the main parachute deployed.<\/p>\n
Descending under parachute, the IXV was safed two minutes after the main chute deployed, with splashdown in the Pacific Ocean occurring slightly ahead of the one hour and forty two minutes mission elapsed time scheduled timeline.<\/p>\n
![\"2014-07-03](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2014\/07\/2014-07-03-19_27_48-Space-in-Images-2014-06-IXV-hoisted-aboard-350x232.jpg\")
The IXV deployed floatation balloons to keep itself on the surface for recovery by ship.<\/p>\nWednesday\u2019s launch was the first of the year for Arianespace whose next mission will be the deployment of two Galileo navigation satellites via Russia\u2019s Soyuz rocket on 27 March.<\/p>\n
The next Vega launch, carrying the Sentinel-2A Earth science satellite for ESA, is scheduled for mid-June while a further mission is scheduled for September with the LISA Pathfinder technology demonstration mission, also for ESA.<\/p>\n
(Images via ESA)<\/p>\n","protected":false},"excerpt":{"rendered":"
The European Space Agency is flying a reentry demonstration mission Wednesday with its Intermediate Experimental Vehicle (IXV). Boosted by Europe\u2019s lightweight Vega rocket, the IXV flew a suborbital mission culminating in landing and recovery in the Pacific Ocean after around 102 minutes of flight. Liftoff is occurred at 13:40 UTC from Kourou, French Guiana. VEGA […]<\/p>\n","protected":false},"author":1,"featured_media":30338,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[246,4151,1311],"class_list":["post-39402","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-esa","tag-ixv","tag-vega"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39402"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=39402"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39402\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30338"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=39402"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=39402"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=39402"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}