BEGIN:VCALENDAR VERSION:2.0 PRODID:-//chikkutakku.com//RDFCal 1.0//EN X-WR-CALDESC:GoogleカレンダーやiCalendar形式情報を共有シェ アしましょう。近所のイベントから全国のイベントま で今日のイベント検索やスケジュールを決めるならち っくたっく X-WR-CALNAME:ちっくたっく X-WR-TIMEZONE:UTC BEGIN:VEVENT SUMMARY:Falcon 9 B5 • CAS500 2 DTSTART;VALUE=DATE-TIME:20260503T065900Z DTEND;VALUE=DATE-TIME:20260503T073600Z UID:104765161026 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch several smallsats on a rideshare mission to Sun-synchronous orbit. Main payload is the CAS5 00 2 satellite.\n-\nThe South Korean CAS500 (Compact Advanced Satellite 50 0) Earth-observation satellites will image the Earth in panchromatic and m ultispectral modes using the AEISS-C (Advanced Earth Imaging Sensor System ) payload. They have a launch mass of ~500kg and a designed service life o f 4 years.\n\nWebcast: https://x.com/i/broadcasts/1AKEmODRWpZKL\nhttps://w ww.spacex.com/launches/cas500-2\n\nhttps://spaceflightnow.com LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) GYUB • TBD DTSTART;VALUE=DATE-TIME:20260505T050000Z DTEND;VALUE=DATE-TIME:20260505T090000Z UID:852439048158 DESCRIPTION:An Korean Ministry of National Defense (ADD) rocket launched o n its second orbital flight. It will lift off from a sea platform in the S outh China Sea\, just 4km south of Jeju Island\, and will place a small sy nthetic aperture radar (SAR) prototype satellite for Hanwha into orbit. T he four stage launcher doesn't have a public name and is known as Solid Fu el Space Launcher (고체연료 우주발사체\, Goche Yeollyo Uju Balsac he\, GYUB). It uses solids for three stages and liquid propulsion on the f ourth stage.\n-\nDelayed from early 2026\, Apr. 22 and 25.\n\nWebcast: htt ps://www.youtube.com/live/jR2pzFAVe-U LOCATION:Südchinesisches Meer END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-10B • Test Flight DTSTART;VALUE=DATE:20260505 DTEND;VALUE=DATE:20260506 UID:179922645845 DESCRIPTION:A China Rocket (CALT) Long March (Chang Zheng) CZ-10B rocket will launch on its first test flight. The first stage is powered by seven YF-100N keroLOX engines\, the second stage is propelled by a YF-219 methaL OX engine. The first stage is reusable and will attempt a landing on the d rone ship Linghangzhe (领航者)\, via its tension wires recovery system on its deck.\n-\nDelayed from Apr. 5\, 19 and late April. LOCATION:Pad 2 - Hainan Commercial Launch Site https://maps.app.goo.gl/nGf kosKTdhF5khDg8 END:VEVENT BEGIN:VEVENT SUMMARY:Falcon 9 B5 • Starlink DTSTART;VALUE=DATE-TIME:20260506T020000Z DTEND;VALUE=DATE-TIME:20260506T020000Z UID:147340682747 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch a batch of 25 Sta rlink v2 Mini Optimized satellites into low Earth orbit. This flight is in ternally known as Starlink Group 17-29 and the booster is designated as B 1081.24 for this mission\, flying with a reused fairing.\n-\nStarlink v2 M ini Optimized satellites are built by SpaceX and have a reported launch ma ss of 575kg. The mass-produced spacecraft carry a communications payload u sing the Ku and Ka frequency bands\, plus E-band for backhaul\, which will allow Starlink to provide ~4x more capacity per satellite than earlier it erations. They also employ optical inter-satellite links\, phased array be am forming and digital processing technologies. On the v2 sats the Krypton thrusters are replaced with new and more powerful Argon Hall thrusters. T he Optimized chassis features upgrades\, such as a new backhaul antenna wi th a SpaceX-designed and built dual-band chip and improved avionics\, prop ulsion and power systems. Starlink sats are able to track on-orbit debris and capable of autonomous collision avoidance. All satellites will be equi pped with anti-reflective coatings.\nThe updated Starlink network architec ture has 1584 satellites at 550km altitude and an inclination of 53 degree s\, 1584 satellites at 540km and an inclination of 53.2 degrees\, 720 sate llites at 570km and an inclination of 70 degrees\, and 520 satellites at 5 60km and an inclination of 97.6 degrees. The initial FCC application cover ed 4408 Starlink satellites. Eventually SpaceX will launch and operate a f ollow-on network of 7518 additional Starlink satellites transmitting in V- band frequencies. In the final deployment stage an additional 30000 Starli nk satellites might get orbited.\n\nWebcast: \nhttps://www.spacex.com/lau nches/sl-17-29\n\nhttps://spaceflightnow.com/ LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:Long March CZ-7 • Tianzhou 10 DTSTART;VALUE=DATE-TIME:20260509T230000Z DTEND;VALUE=DATE-TIME:20260509T230000Z UID:363966066978 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-7 rocket will launch the tenth Tianzhou (TZ-10) cargo c raft for docking with the China Space Station (CSS). The Tianzhou 10 (天 舟 or "heavenly vessel") craft will operate for about 9 months in space.\ n-\nDelayed from Jan. 31\, Feb. 15 and Apr. 14. LOCATION:Pad 201 - Wenchang Satellite Launch Center https://goo.gl/maps/7v 4maqUT9VigBvQr5 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Super Heavy B3 • IFT-12 Starship B3 DTSTART;VALUE=DATE-TIME:20260512T223000Z DTEND;VALUE=DATE-TIME:20260512T223000Z UID:120993391278 DESCRIPTION:A SpaceX Super Heavy rocket will launch a Starship prototype o n its eleventh test flight\, designated IFT-12 (Integrated Flight Test). S tarship will be a stretched version equipped with Raptor 3 engines and per form a payload deployment test with 8? Starlink v3 simulators and a religh t of a single Raptor engine while in space. Super Heavy will also use Rapt or 3 engines and perform a RTLS landing at the launch tower. It will have have an integrated vented interstage/forward dome\, three grid fins instea d of the prior four\, as well as the use of the grid fins as catch points. The booster/ship combination is designated as B19/S39\, both of the Block 3 variant.\n-\nDelayed from March and April.\n\nWebcast:\nhttps://www.spa cex.com/launches/starship-flight-12 LOCATION:Orbital Launch Pad 2\, 54018 TX-4\, Brownsville\, TX 78521\, Vere inigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • SpX-34 Dragon 2 CRS2 DTSTART;VALUE=DATE-TIME:20260512T230000Z DTEND;VALUE=DATE-TIME:20260512T230000Z UID:965684142795 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch the latest Dragon 2 spacecraft on an operational cargo delivery mission to the Internationa l Space Station. The flight is being conducted under the second phase of t he Commercial Resupply Services (CRS) contract with NASA. Total cargo mass is ?kg\, including ?. B10XX.X is the Falcon 9 booster flying this mission and Dragon is vehicle C209.6 on this flight. The first stage will perform a RTLS landing at LZ-40.\n-\nMoved forward from June 2026. Delayed from Q 4 and March.\n\nWebcast:\nhttps://www.spacex.com/launches/crs34\n\nhttps:/ /spaceflightnow.com LOCATION:SpaceX LC-39A\, Florida\, USA END:VEVENT BEGIN:VEVENT SUMMARY:Vega C • SMILE DTSTART;VALUE=DATE-TIME:20260519T035200Z DTEND;VALUE=DATE-TIME:20260519T035200Z UID:227318551276 DESCRIPTION:An Avio Vega C rocket\, designated VV29\, will launch ESA's & CAS' SMILE mission into a highly elliptical orbit. The Solar wind Magnetos phere Ionosphere Link Explorer (SMILE) is a joint initiative between ESA a nd the Chinese Academy of Sciences. The 2.3 tonne spacecraft will study Ea rth’s magnetic environment on a global scale. The aim of the mission is to build a more complete understanding of the Sun-Earth connection. ESA is providing the payload module\, launch vehicle\, and one of the scientific instruments for SMILE\, while CAS is responsible for three scientific ins truments and the mission and science operations. For a few weeks post-laun ch\, SMILE will gradually propel itself into its science-performing orbit of 121000 x 5000km. This is the first mission handled by Avio as launch pr ovider.\n\nMission profile video: https://youtu.be/QmuxhO7o3kA\n-\nDelayed from April 2025\, September and Apr. 9.\n\nWebcast: https://www.youtube.c om/live/6q8aKbcKCOs\nwatch.esa.int LOCATION:ELV\, 66PG+C22\, Carbet Toukan 97310\, Französisch-Guyana END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • StriX 9 DTSTART;VALUE=DATE:20260522 DTEND;VALUE=DATE:20260523 UID:271410017047 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie kickstage wil l launch the newest StriX satellite for Synspective\, its ninth sat after StriX α\, β\, 1\, 3\, 4\, 2\, 5 and 6. Rocket Lab's mission will be name d "Viva La Strix" and will use a customized fairing.\n-\nStriX are Japanes e synthetic aperture radar satellites built by Synspective for their plann ed 25 satellite constellation. They feature an X-band synthetic aperture r adar. The 100kg StriX operational satellites are more light weight than th e 150kg StriX α and β prototypes. The satellites feature two deployable panes\, one side carrying solar cells\, the other carrying the X-band rada r antenna.\nSynspective is planning a constellation of 25 satellites that can target data with a ground resolution of 1-3m\, single polarized (VV)\, and a swath width of more than 10-30km. The StriX observation modes are S tripmap and Sliding Spotlight mode and each satellite has an SAR antenna t hat is 5 meters in length and stowed during launch. The simple design of t he satellites allows for affordable development of the constellation.\n\nW ebcast: \nhttps://rocketlabcorp.com/live-stream/ LOCATION:Onenui Station\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Atlas V 551 • Amazon Leo DTSTART;VALUE=DATE:20260522 DTEND;VALUE=DATE:20260523 UID:140833453279 DESCRIPTION:A United Launch Alliance Atlas V rocket\, designated AV-?\, wi ll launch a batch of 29 operational satellites for the Amazon Leo constell ation. The mission is known as Leo 7 by ULA and LA-07 by Amazon. Total pay load mass will be ~16.7 tonnes. Atlas will deploy the satellites in an ini tial orbit of 450km altitude\, the satellites will then use their electric propulsion systems to settle into their assigned final orbits. The Amazon Leo constellation will enable Internet service for customers between 56 d egrees north and south latitude. Atlas will fly in the 551 vehicle configu ration with a five-meter medium length fairing\, five GEM-63 solid rocket boosters and a single-engine Centaur upper stage.\n\nMission profile video : https://youtu.be/ZATwTLIbQu8\n-\nOperational satellites of the Amazon Le o constellation (formerly known as Project Kuiper) are a significant upgra de from the two prototype satellites of the Kuiper Protoflight mission. Th e ~572kg satellites are equipped with Hall-effect thruster technology for propulsion. They feature improved systems and sub-systems on board\, inclu ding phased array antennas\, processors\, solar arrays\, propulsion system s\, and optical inter-satellite links. In addition\, the satellites are co ated in a dielectric mirror film unique to Amazon Leo that scatters reflec ted sunlight to help make them less visible to ground-based astronomers. A mazon Leo is planned to work in concert with Amazon's network of 12 satell ite ground station facilities. In addition to connecting to ground station s\, satellites will interconnect via optical infrared laser connections. A mazon refers to this technology as OISL (optical inter-satellite link).\nT he Amazon Leo constellation is planned to consist of 3236 satellites opera ting in 98 orbital planes in three orbital shells\, one each at 590km\, 610km and 630km orbital altitude. Kuiper satellites will fly in mid-incli nation orbits\, enabling Internet service for customers between 56 degrees north and south latitude. Phase 1 of deployment will be 578 satellites at 630km altitude and an orbital inclination of 51.9 degrees. A total of fiv e phases of constellation development are planned.\n-\nMoved forward from June.\n\nWebcast: \nhttps://www.ulalaunch.com/missions/next-launch/atlas- v-amazon-leo-7\n\nhttps://spaceflightnow.com LOCATION:Cape Canaveral AFS Launch Complex 41\, Titan III Rd\, Titusville\ , FL 32780\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-2F/G • Shenzhou 23 DTSTART;VALUE=DATE:20260525 DTEND;VALUE=DATE:20260526 UID:194913394697 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h 2F/G rocket will launch the Shenzhou 23 spacecraft\, a crewed mission to dock with the orbiting China space station CSS. ?\, ? and ? will launch o n China's latest crewed space mission. One astronaut will stay for a year- long mission.\n-\nMoved forward from late October and June. LOCATION:LC-43/91 (Pad 921 / South Launch Site 1) - Jiuquan Satellite Laun ch Center https://goo.gl/maps/7v4maqUT9VigBvQr5 END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Electron • QPS-SAR 16 DTSTART;VALUE=DATE:20260525 DTEND;VALUE=DATE:20260526 UID:114211446530 DESCRIPTION:A Rocket Lab Electron rocket topped with a Curie upper stage w ill launch the QPS-SAR 16 satellite (named ?) for iQPS of Japan. Rocket L ab's mission will be named "The Grain Goddess Provides" and fly with an ex tended fairing.\n-\nQ-shu Pioneers of Space – Synthetic Aperture Radar ( QPS-SAR) are operational satellites in a series of small high-resolution S AR (synthetic aperture radar) Earth observation sats by the QPS Institute (iQPS). The 100kg satellites feature a 3.6m diameter antenna of only 10kg. It can distinguish objects 1 meter long and identify cars on the road. Co mpared to the prototypes (QPS-SAR 1\, 2)\, these satellites have increased power due to two deployable solar arrays and increased battery capacity. They also feature thrusters for station keeping. The planned constellation will have 36 satellites.\n\nWebcast: \nhttps://rocketlabcorp.com/mission s/ LOCATION:Onenui Station\, Māhia 4198\, Neuseeland END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-7A • TBD DTSTART;VALUE=DATE:20260526 DTEND;VALUE=DATE:20260527 UID:338783851503 DESCRIPTION:A China Academy of Launch Vehicle Technology (CALT) Long Marc h (Chang Zheng) CZ-7A rocket will launch an unknown payload into orbit.\n- \nDelayed from late January and early March. LOCATION:Pad 201 - Wenchang Satellite Launch Center https://goo.gl/maps/7v 4maqUT9VigBvQr5 END:VEVENT BEGIN:VEVENT SUMMARY:Busy DTSTART;VALUE=DATE:20260531 DTEND;VALUE=DATE:20260601 UID:325814222901 DESCRIPTION:Busy LOCATION: END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Ariane 62 • MTG-I 2 DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:174029713192 DESCRIPTION:Arianespace will launch an Ariane 6 rocket on a flight designa ted VA2XX\, to put the MTG-I 2 meteorological satellite into geosynchronou s transfer orbit. The Meteosat Third Generation Imager satellite will pro vide weather imagery over Europe for the European weather satellite agency \, Eumetsat. Ariane 6 will fly in the Ariane 62 configuration\, using 2 so lid rocket boosters.\n-\nMTG-I 2 is the third satellite in the 3rd generat ion series of Meteosat. It is built on the SmallGEO (LUXOR) bus of OHB wit h Thales Alenia Space instruments and weighs about 3.76 tonnes. MTG (Met eosat Third Generation) is the follow-up system to the Meteosat MSG ser ies of geostationary satellites. MTG will consist of a twin configuration of 3-axis-stabilised satellites: the Imaging mission satellite (MTG-I) an d the Sounding mission satellite (MTG-S). The payload for MTG-I consists of the Flexible Combined Imager (FCI)\, Lightning Imager (LI)\, Data Colle ction System (DCS)\, and search and rescue (GEOSAR). The FCI is expected to outperform MSG Spinning and Enhanced Visible and Infrared Imager (SEVIR I) observations on cloud\, aerosol\, moisture and fire by adding new chann els in the solar domain and by improving temporal-\, spatial-\, and radiom etric resolution. For instance\, the FCI in its High Resolution Fast Image ry mode focusing on Europe/North Africa with a resolution down to 500 met ers and a repeat cycle of 2.5 minutes will produce the greatest benefits t o Nowcasting services. The IRS will provide breakthrough measurements on the time evolution of horizontal and vertical water vapour and temperature structures. It is an unprecedented source of information on the dynamic a nd thermodynamic atmospheric fields\, an important benefit to the Nowcasti ng and Numerical Weather Prediction services. It will also support forecas ting pollution and monitoring of atmospheric minor constituents through it s capability to provide estimates of diurnal variations of tropospheric co ntributions of atmospheric trace gases like ozone and carbon monoxide. Th e LI mission will deliver continuously and simultaneously measurements on total lightning over the full disk\, improving the quality of information essential for Nowcasting services\, for instance early warning of severe w eather and air traffic routing and safety. The LI is therefore expected to contribute significantly to risk reduction measures. It will also contrib ute to the remote sensing of precipitation and support environmental appli cations related to the atmospheric chemical processes and to the climate s ystem.\n\nWebcast:\nhttps://www.arianespace.com/road-to-space/ LOCATION:ELA4 (l'Ensemble de Lancement Ariane 6) - Centre Spatial Guyanais \, Französisch-Guyana END:VEVENT BEGIN:VEVENT SUMMARY:(NET) New Glenn 7×2 • Amazon Leo DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:673129948063 DESCRIPTION:A Blue Origin New Glenn rocket will launch on its fifth? fligh t\, carrying a batch of 49 operational satellites for Amazon's Kuiper cons tellation. The constellation will number 3236 satellites\, spread out in 9 8 orbital planes\, or pathways\, crisscrossing the planet at an average al titude of about 610km. In its license application with the Federal Communi cations Commission\, Amazon said the Kuiper satellites will fly in mid-inc lination orbits\, enabling Internet service for customers between 56 degre es north and south latitude. New Glenn version 7×2 is equipped with seven BE-4 LNG/LOX engines on the reusable GS1 first stage and two BE-3U hydroL OX engines on the GS2 second stage.\n-\nDelayed from late 2024 and Septemb er. LOCATION:Space Launch Complex 36\, air force station\, Cape Canaveral\, FL 32920\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Gravity YL-2 • Test Flight DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:246162688009 DESCRIPTION:An Orienspace Gravity 2 rocket will perform its first flight.  Gravity 2 (引力二号 or Yinli 2) is equipped with a recoverable first stage propelled by nine Yuanli-110 (Force-110) keroLOX engines and a seco nds stage using one Yuanli-110 vacuum optimized engine. The first stage is equipped with gridfins & landing legs and can be enhanced with expendable solid boosters.\n-\nDelayed from December and September 2025. LOCATION:Hainan Commercial Launch Site END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Long March CZ-10A • Test Flight DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:799093180410 DESCRIPTION:A China Aerospace Science and Technology Corporation (CASC) Lo ng March (Chang Zheng) CZ-10A rocket will launch on its first operational flight as a pathfinder for the crewed CZ-10 rocket. The CZ-10A will also b e used as a cargo variant of the CZ-10 launcher. The first stage is powere d by seven YF-100N keroLOX engines\, while the second-stage is equipped wi th one vacuum-optimized YF-100M engine.\n-\nDelayed from late 2025. LOCATION:Pad 301 - Wenchang Satellite Launch Center END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Nova • Test Flight DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:132815314139 DESCRIPTION:A Stoke Space Nova rocket will launch on its maiden flight. Th e LNG/hydroLOX fueled rocket will feature a reusable first stage powered b y seven Zenith Full Flow Staged Combustion Cycle LNG engines and a second stage propelled by a revolutionary hydroLOX ring aerospike engine.\n-\nDel ayed from 2025. LOCATION:Cape Canaveral AFS Launch Complex 14\, Cape Canaveral\, Florida 3 2920\, Vereinigte Staaten END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Pegasus XL • Link DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:266697444121 DESCRIPTION:A Northrop Grumman Pegasus XL rocket will air-launch from its L-1011 "Stargazer" carrier aircraft to deploy the Swift Reboost mission of Katalyst for NASA in orbit. Swift's orbit has decayed considerably over t he years\, from an initial 600km to about 400km. Its descent is accelerati ng due to atmospheric drag and it would experience reentry around the end of 2026\, so a rescue mission was designed. The Katalyst spacecraft\, name d Link\, will head to an orbit similar to that of Swift\, then spend two t o three weeks closing in on the observatory. The boost vehicle will inspec t its target and once its state is understood\, the rescuer\, which is abo ut 1.5m tall and weighs 350kg\, will close in and capture Swift using its three robotic arms. This will be challenging\, as the NASA observatory was not designed to be serviced. After a successful capture\, the Katalyst sp acecraft will haul Swift back up to its initial altitude of ~600km\, which will boost its lifetime by another ~20 years. The Swift observatory was b uilt by Orbital Sciences\, a company that in 2014 became Orbital ATK\, whi ch was then acquired by Northrop Grumman in 2018. The triple-engine carrie r aircraft is expected to take off about an hour before launch time. LOCATION:Bucholz Army Airfield\, Kwajalein Atoll\, Marshallinseln END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Vega C • IRIDE DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:334085824865 DESCRIPTION:An Avio Vega C rocket\, designated VV?\, will launch the secon d batch of IRIDE Earth observation satellites for The Italian Space Agency ASI and ESA. The 11 satellites on this flight are designated IRIDE-HYP-PL ATINO 1–2\, IRIDE-MS1-EAGLET2 11\, IRIDE-SAR-NIMBUS 1–6\, IRIDE-SAR-NO X 1 and IRIDE-VHR-NIMBUS 1. IRIDE is a space-based observation program in itiated under the framework of Italy's National Recovery and Resilience Pl an (PNRR). IRIDE will be unique in its incorporation of a wide range of se nsing techniques and technologies\, including microwave imaging with Synth etic Aperture Radars (SAR)\, optical imaging at high and medium resolution s\, and coverage across panchromatic\, multispectral\, hyperspectral\, and infrared bands. Once operational\, IRIDE will be used to track the impact s of climate change and provide data to support startups and SMEs in creat ing commercial applications. Also aboard this launch are a number of Prom éthée satellites for the Japetus constellation. This mission is the firs t flight of Vega under the new management of Avio.\n-\nDelayed from Octobe r 1 and Q4 2025. LOCATION:ELV\, 66PG+C22\, Carbet Toukan 97310\, Französisch-Guyana END:VEVENT BEGIN:VEVENT SUMMARY:(NET) New Glenn 7×2 • Blue Moon MK1 Pathfinder CLPS DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:241453502709 DESCRIPTION:A Blue Origin New Glenn rocket will launch on its third? fligh t\, carrying the Blue Moon Mark 1 Pathfinder\, designated MK1-SN001 and na med Endurance\, to a lunar landing. NASA will fly a camera system to study how engine plumes interact with regolith at south polar regions of the mo on\, collecting data to support future crewed landing missions. The payloa d\, called Stereo Cameras for Lunar Plume Surface Studies (SCALPSS)\, will fly through NASA’s Commercial Lunar Payload Services (CLPS) program. Th e spacecraft is 8.05m tall with a diameter of 3.08m and has a wet mass (fu lly fuelled) of up to 21350kg. New Glenn will place Blue Moon into low Ear th orbit\, remaining there for three to four orbits to do initial checkout s. It will then raise its apogee for additional tests\, including its high -gain antenna system\, before performing a translunar injection maneuver t o go to the Moon\, entering a low lunar orbit five to seven days later. Th e spacecraft will conduct multiple subsystem characterisation activities i n lunar orbit before attempting a landing. Powered by a single hydroLOX-fu eled BE-7 engine\, the lander will aim to touch down within 10m of its int ended target at Shackleton crater. New Glenn version 7×2 is equipped with seven BE-4 LNG/LOX engines on the reusable GS1 first stage and two BE-3U hydroLOX engines on the GS2 second stage.\n-\nDelayed from March\, June\, August and late 2025. LOCATION:Space Launch Complex 36\, air force station\, Cape Canaveral\, FL 32920\, USA END:VEVENT BEGIN:VEVENT SUMMARY:(NET) Falcon 9 B5 • Transporter-17 DTSTART;VALUE=DATE:20260601 DTEND;VALUE=DATE:20260602 UID:191141264576 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch several smallsats on the Transporter-17 rideshare mission to Sun-synchronous orbit.\n\nWebc ast: \nhttps://www.spacex.com/launches\n\nhttps://spaceflightnow.com LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT END:VCALENDAR