LEO (wahana antariksa): Perbedaan antara revisi
Tampilan
Konten dihapus Konten ditambahkan
k NFarras memindahkan halaman LEO (pesawat luar angkasa) ke LEO (wahana antariksa) |
Tidak ada ringkasan suntingan |
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{{Infobox spaceflight |
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'''LEO''' ('''Lunarer Erkundungsorbiter'''; Inggris: Lunar Exploration Orbiter) adalah nama dari sebuah misi yang diusulkan Jerman ke Bulan, diumumkan oleh German Aerospace Center (DLR) Direktur Walter Doellinger pada 2 Maret 2007. Karena membutuhkan uang untuk tahun 2009 maka dialihkan di tempat lain, awal proyek ini ditunda tanpa batas waktu. |
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| name = Pengorbit Bulan |
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| names_list = LEO<!--list of previous names if the spacecraft has been renamed. |
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Include the dates applicable if possible, and separate each name with a linebreak. |
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Omit if the spacecraft has only ever been known by one name. |
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Do not include Harvard, COSPAR/NSSDC or SATCAT/NORAD/NASA designations as alternative names--> |
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<!--image of the spacecraft/mission--> |
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| image = <!--omit the "file" prefix--> |
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| image_caption = <!--image caption--> |
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| image_alt = <!--image alt text--> |
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| image_size = <!--include px/em; defaults to 220px--> |
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<!--Basic details--> |
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| mission_type = <!--eg. Technology, Reconnaissance, ISS assembly, etc--> |
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| operator = [[German Aerospace Center]] |
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| Harvard_designation = <!--spacecraft launched 1962 and earlier only (eg. 1957 Alpha 2)--> |
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| COSPAR_ID = <!--spacecraft launched since 1963 only (aka NSSDC ID; eg. 1998-067A)--> |
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| SATCAT = <!--satellite catalogue number, omit leading zeroes (e.g. 25544)--> |
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| website = <!--Homepage of the craft/mission, OFFICIAL PAGES ONLY--> |
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| mission_duration = 4 tahun (rencana)<!--How long the mission lasted--> |
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| distance_travelled = <!--How far the spacecraft travelled (if known)--> |
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| orbits_completed = <!--number of times the spacecraft orbited the Earth - see below for spacecraft beyond Earth orbit--> |
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| suborbital_range = <!--downrange distance reached if spacecraft did not enter orbit--> |
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| suborbital_apogee = <!--altitude reached if spacecraft did not enter orbit--> |
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<!--Spacecraft properties--> |
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| spacecraft = <!--Spacecraft name/serial number (eg. Space Shuttle ''Discovery'', Apollo CM-118), etc--> |
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| spacecraft_type = <!--eg. GPS Block II, Kobalt-M, US-K, etc--> |
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| spacecraft_bus = <!--eg. A2100M, Star-2, etc--> |
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| manufacturer = <!--company or companies who built the satellite--> |
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| launch_mass = ~{{convert|650|kg|abbr=on}} termasuk sub satellite |
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| BOL_mass = <!--spacecraft mass in orbit at beginning of operational life, after LEOP phase--> |
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| landing_mass = <!--Mass after landing (recovered spacecraft only)--> |
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| dry_mass = <!--spacecraft mass in orbit without fuel--> |
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| payload_mass = <!--Mass of cargo carried by spacecraft (eg. for Space Shuttle), or total mass of instrumentation/equipment/experiments for mission--> |
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| dimensions = <!--body dimensions and solar array span--> |
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| power = <!--end-of-life power, in watts--> |
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<!--Launch details--> |
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| launch_date = 2012 (rencana)<!--{{start date|YYYY|MM|DD|hh|mm|ss|TZ=Z}}--> |
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| launch_rocket = <!--Rocket that launched the satellite, include upper stage if distinct from rocket* and if possible flight/tail/serial number--> |
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| launch_site = <!--Where the rocket launched from, including complex and pad; do not include the full address or country--> |
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| launch_contractor = <!--organisation(s) that conducted the launch (eg. United Launch Alliance, Arianespace, etc)--> |
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| deployment_from = <!--place where deployed from--> |
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| deployment_date = <!--date deployed--> |
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| entered_service = <!--date on which the spacecraft entered service, if it did not do so immediately after launch--> |
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<!-- * - e.g. Proton-M/Briz-M not Proton-M, but Titan IV(401)A not Titan IV(401)A-Centaur--> |
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<!--end of mission--> |
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| disposal_type = <!--Whether the spacecraft was deorbited, decommissioned, placed in a graveyard orbit, etc--> |
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| deactivated = <!--when craft was decommissioned--> |
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| destroyed = <!--when craft was destroyed (if other than by re-entry)--> |
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| last_contact = <!--when last signal received if not decommissioned--> |
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| recovery_by = <!--recovered by--> |
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| recovery_date = <!--recovery date--> |
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| decay_date = <!--when craft re-entered the atmosphere, not needed if it landed--> |
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| landing_date = <!--when the spacecraft made a controlled landing, not needed if it did not return intact--> |
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| landing_site = <!--where the craft landed; site/runway or coordinates--> |
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<!-- |
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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. |
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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. |
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{{end date|YYYY|MM|DD|hh|mm|ss|TZ=Z}} (for Zulu/UTC) or {{end date|YYYY|MM|DD}} (if time unknown) |
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--> |
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<!--orbit parameters--> |
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<!--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--> |
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| orbit_reference = [[Orbit selenosentris|Selenosentris]] |
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| orbit_regime = <!--high, low, medium, molniya, GSO - please link (e.g. [[Low Earth orbit|Low Earth]] - please don't use acronyms--> |
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| orbit_longitude = <!--geosynchronous satellites only--> |
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| orbit_slot = <!--Designation of orbital position or slot, if not longitude (e.g plane and position of a GPS satellite)--> |
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| orbit_semimajor = <!--semimajor axis--> |
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| orbit_eccentricity = <!--orbital eccentricity--> |
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| orbit_periapsis = {{convert|50|km|abbr=on}} |
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| orbit_apoapsis = <!--apoapsis altitude--> |
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| orbit_inclination = <!--orbital inclination--> |
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| orbit_period = <!--time taken to complete an orbit--> |
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| orbit_RAAN = <!--right ascension of the ascending node--> |
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| orbit_arg_periapsis = <!--argument of perigee/periapsis--> |
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| orbit_mean_anomaly = <!--mean anomaly at epoch, only use in conjunction with an epoch value--> |
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| orbit_mean_motion = <!--mean motion of the satellite, usually measured in orbits per day--> |
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| orbit_repeat = <!--repeat interval/revisit time--> |
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| orbit_velocity = <!--speed at which the spacecraft was travelling at epoch - only use for spacecraft with low orbital eccentricity--> |
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| orbit_epoch = rencana |
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| orbit_rev_number = <!--revolution number--> |
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| apsis = selene |
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<!--transponder parameters--> |
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| trans_band = <!--Transponder frequency bands--> |
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| trans_frequency = <!--specific frequencies--> |
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| trans_bandwidth = <!--bandwidth--> |
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| trans_capacity = <!--capacity of the transponders--> |
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| trans_coverage = <!--area covered--> |
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| trans_TWTA = <!--TWTA output power--> |
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| trans_EIRP = <!--equivalent isotropic power--> |
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| trans_HPBW = <!--half-power beam width--> |
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<!--Only use where a spacecraft/mission is part of a clear programme of sequential missions. |
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If in doubt, leave it out--> |
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| programme = |
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| previous_mission = |
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| next_mission = |
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<!--mission insignia or patch--> |
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| insignia = <!--omit the "file" prefix--> |
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| insignia_caption = <!--image caption--> |
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| insignia_alt = <!--image alt text--> |
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| insignia_size = <!--include px/em; defaults to 180px--> |
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}} |
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'''LEO''' ('''Lunarer Erkundungsorbiter'''; Inggris: Lunar Exploration Orbiter) adalah nama dari sebuah misi yang diusulkan Jerman ke Bulan, diumumkan oleh German Aerospace Center (DLR) Direktur Walter Doellinger pada 2 Maret 2007. Karena pendanaan untuk tahun 2009 dialihkan ke sektor lainnya, misi ini ditunda hingga waktu yang tidak ditentukan. |
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== Referensi == |
== Referensi == |
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* [http://www.dw-world.de/dw/article/0,2144,2370335,00.html Germany Mulls Sending Own Mission to the Moon. Deutsche Welle 04.03.2007] |
* [http://www.dw-world.de/dw/article/0,2144,2370335,00.html Germany Mulls Sending Own Mission to the Moon. Deutsche Welle 04.03.2007] |
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{{wahanaantariksa-stub}} |
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[[Kategori:Misi ke Bulan]] |
[[Kategori:Misi ke Bulan]] |
Revisi per 9 Juli 2020 07.30
Nama | LEO |
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Operator | German Aerospace Center |
Durasi misi | 4 tahun (rencana) |
Properti wahana | |
Massa luncur | ~650 kg (1.430 pon) termasuk sub satellite |
Awal misi | |
Tanggal luncur | 2012 (rencana) |
Parameter orbit | |
Sistem rujukan | Selenosentris |
Ketinggian periselene | 50 km (31 mi) |
Epoch | rencana |
LEO (Lunarer Erkundungsorbiter; Inggris: Lunar Exploration Orbiter) adalah nama dari sebuah misi yang diusulkan Jerman ke Bulan, diumumkan oleh German Aerospace Center (DLR) Direktur Walter Doellinger pada 2 Maret 2007. Karena pendanaan untuk tahun 2009 dialihkan ke sektor lainnya, misi ini ditunda hingga waktu yang tidak ditentukan.