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 • Transporter-15 DTSTART;VALUE=DATE-TIME:20251119T181800Z DTEND;VALUE=DATE-TIME:20251119T191500Z UID:309532747570 DESCRIPTION:A SpaceX Falcon 9 Block 5 rocket will launch several smallsats on the Transporter-15 rideshare mission to Sun-synchronous orbit. Onboard is LEO Express 3\, which is a Mira OTV (Orbital Tug Vehicle) by Impulse Space. Part of the payloads is also ESA's second Earth observation Scout m ission\, HydroGNSS\, which will provide measurements of key hydrological c limate variables\, including soil moisture\, freeze–thaw state over perm afrost\, inundation and wetlands\, and above-ground biomass\, using a tech nique called Global Navigation Satellite System (GNSS) reflectometry. The satellite measures the signal reflected off the land\, ice and ocean from existing GNSS missions such as Galileo and GPS. Although these signals are faint\, they can be collected by a low power receiver that can be accommo dated on a small satellite in low Earth orbit making it compatible with a Scout mission. The mission will complement missions such as ESA's SMOS and Biomass\, Copernicus Sentinel 1 and NASA's SMAP. The ION-SCV Stellar Step hanus and Galactic Giorgius CubeSat Carriers\, the Mauve space telescope a nd 8 IRIDE satellites for Italy's ASI (IRIDE-MS1-EAGLET2 1–8) will also be on this flight. Onboard is also Winnebago 5\, which is an orbital fac tory with reentry capsule for Varda Space. Further payloads are YAM 9\, FO RMOSAT 8A\, Pelican 5–6\, Umbra 11\, NewSat 47 & NewSat 51–52\, Accent ure 1\, AC1 001–003\, AE5Ra/b/c\, ANISCSAT\, HUNITY\, SARI 1–2\, Black Kite 1\, BRO 17\, BRO 20\, CTC 1A/B/C\, FGN-TUG-S01\, GENA-OT 1\, GYEONGG ISat 1\, HCT-Sat 2\, IHI-Sat 2\, Lilium 2–3\, LUNA 1\, Mercury One (Merc ury 1)\, MICE 1\, Nahla\, OTTER\, PHASMA-LAMARR\, PHASMA-DIRAC\, PHI 1\, P IAST-M\, PIAST-S1\, PIAST-S2\, PW6U\, Rapid\, Reduced-cost high-Risk Resea rch (R5)\, SpeQtre\, SPiN 2\, T.MicroSat 1\, TORO 2\, TRYAD 1–2\, Veery- 0G (Veery v0.5)\, Winnebago 5 (W-Series 5)\, WISDOM A-B\, 3UCubed-A\, 6GSt arLab\, 5 ICEYE X satellites\, 36 Flock 4H SuperDove CubeSats for Planet a nd four Lemur 2 CubeSats for Spire. The booster is designated B10XX.X for this mission and will perform a RTLS (return to launch site) at LZ-4.\n-\n YAM (Yet Another Mission) is a series of micro satellites owned by Loft O rbital\, which host various payloads for different customers. YAM 10 will use Loft Orbital's Longbow satellite\, which is based on the Arrow bus fro m Airbus\, and has a launch mass of 300–500kg. It will carry a high-prec ision Earth imaging payload for EarthDaily Analytics\, who plans a 10 sate llite constellation.\n-\nFORMOSAT 8A is the first satellite of the FORMOS AT 8 Earth observation satellite constellation consisting of six high-res olution optical remote sensing satellites for Taiwan's NSPO. The 380kg sat ellites feature a Hydrogen peroxide propulsion system. The imaging payload features one panchromatic band and at least four multi-spectral bands wit h a ground sampling distance (GSD) in panchromatic band of 1m and in multi -spectral bands of 2m. The swath width is 10km. The FORMOSAT 8 satellites are deployed in the sun-synchronous orbit for multiple daily revisit capab ilities and global coverage of satellite images. Some of the satellites wi ll carry a secondary payload. FORMOSAT 8B will carry a Gamma-ray Transient s Monitor (GTM).\n-\nW-Series (Winnebago) are a series of ~300kg spacecra ft designed by Varda Space Industries\, which will spend up to three month s in orbit to test space manufacturing technologies. At the end of that mi ssion\, a reentry capsule will return to Earth the material produced in or bit.\n-\nPelican satellites are part of the Pelican commercial Earth obser vation constellation by Planet Labs to succeed the SkySat constellation. P elicans have a launch mass of 160kg and is designed to operate in 500km SS O. Up to 30 satellites are planned for the Pelican constellation.\n-\nION- SVC (InOrbit NOW) CubeSat Carriers\, developed by Italian company D-Orbit\ , are 150kg free flying orbital tugs and technology demonstrators\, which will host experiments and CubeSats to be deployed once in orbit.\n-\nFinni sh firm ICEYE continues to expand its constellation with Generation 3 comp act SAR microsatellites\, each with a mass of around 90kg. They are Gen3 s ats for a constellation of SAR (Synthetic Aperture Radar) equipped microsa tellites. ICEYE provides near-real-time SAR imagery and the radar instrume nt can image through clouds\, obscuring weather and darkness.\n-\nUmbra (U mbra-SAR) are a 65kg satellites and equipped with a X-band SAR (synthetic aperture radar) to capture snapshot imagery with a resolution of 25 centim eters over a 16 square km area. The mission is to test technologies and de signs\, validate performance\, and progress into a fully operational archi tecture. To collect radar imagery Umbra has developed a proprietary antenn a technology allowing for relatively low power operation to achieve high q uality SAR images.\n-\nThe Aleph 1 constellation consists of identical Ñu Sat (NewSat) satellites weighing 50kg each. The satellites are equipped wi th an imaging system operating in visible light and infrared. The constell ation will allow for commercially available real-time Earth imaging and vi deo with a ground resolution of 1m. Future constellation concepts present ed by Satellogic call for 90 satellites to achieve a 15-minute revisit tim e along with improvements in spectral\, spatial and radiometric resolution and autonomous processing chains for even quicker turnaround. A 300 satel lite constellation planned could accomplish a 5-minute revisit time.\n-\nI RIDE-MS1-EAGLET2 satellites are part of the IRIDE earth observation const ellation built by the Italian Space Agency ASI with the support of ESA. It will be one of six constellations that make up IRIDE. The payload on the Eaglets is one of two types of Multispectral sensors\, which capture image s with multiple spectral channels on the electromagnetic spectrum\, enabli ng the identification and measurement of different materials\, land cover studies\, vegetation health and crop types.\nIRIDE will be unique in its i ncorporation of a wide range of sensing techniques and technologies\, incl uding microwave imaging with Synthetic Aperture Radars (SAR)\, optical ima ging at high and medium resolutions\, and coverage across panchromatic\, m ultispectral\, hyperspectral\, and infrared bands. Once operational\, IRID E will be used to track the impacts of climate change and provide data to support startups and SMEs in creating commercial applications.\n-\nDelayed from October and Nov. 10.\n\nWebcast: \nhttps://www.spacex.com/launches\n https://spaceflightnow.com LOCATION:Vandenberg AFB Space Launch Complex 4\, Lompoc\, Kalifornien 9343 6\, USA END:VEVENT END:VCALENDAR