LEO (wahana antariksa): Perbedaan antara revisi

Pengorbit Bulan
Nama	LEO
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

Jelajahi riwayat secara interaktif

← Revisi sebelumnya

Konten dihapus Konten ditambahkan

VisualTeks wiki

Sebaris

Revisi terkini sejak 12 Februari 2023 10.17

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.

Referensi[sunting | sunting sumber]

Artikel bertopik wahana antariksa atau satelit ini adalah sebuah rintisan. Anda dapat membantu Wikipedia dengan mengembangkannya.

@@ Baris 1: / Baris 1: @@
+{{Underlinked|date=Februari 2023}}
-'''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.
+{{Infobox spaceflight
+| name                  = Pengorbit Bulan
+| names_list            = LEO<!--list of previous names if the spacecraft has been renamed.
+Include the dates applicable if possible, and separate each name with a linebreak.
+Omit if the spacecraft has only ever been known by one name.
+Do not include Harvard, COSPAR/NSSDC or SATCAT/NORAD/NASA designations as alternative names-->
+<!--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          = <!--eg. Technology, Reconnaissance, ISS assembly, etc-->
+| operator              = [[German Aerospace Center]]
+| 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      = 4 tahun (rencana)<!--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|650|kg|abbr=on}} termasuk sub satellite
+| 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           = 2012 (rencana)<!--{{start date|YYYY|MM|DD|hh|mm|ss|TZ=Z}}-->
+| launch_rocket         = <!--Rocket that launched the satellite, include upper stage if distinct from rocket* and if possible flight/tail/serial number-->
+| launch_site           = <!--Where the rocket launched from, including complex and pad; do not include the full address or country-->
+| launch_contractor     = <!--organisation(s) that conducted the launch (eg. United Launch Alliance, Arianespace, etc)-->
+| 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         = <!--Whether the spacecraft was deorbited, decommissioned, placed in a graveyard orbit, etc-->
+| 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       = [[Orbit selenosentris|Selenosentris]]
+| orbit_regime          = <!--high, low, medium, molniya, GSO - please link (e.g. [[Low Earth orbit|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       = {{convert|50|km|abbr=on}}
+| 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           = rencana
+| orbit_rev_number      = <!--revolution number-->
+| apsis                 = selene
+<!--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-->
+}}
+'''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.
 == Referensi ==
 {{Reflist}}
-*[http://www.reuters.com/article/scienceNews/idUSL0784182620071107?feedType=RSS&feedName=scienceNews&rpc=22&sp=true Germany plans unmanned lunar orbit. Reuters 11.07.2007]
+* [http://www.reuters.com/article/scienceNews/idUSL0784182620071107?feedType=RSS&feedName=scienceNews&rpc=22&sp=true Germany plans unmanned lunar orbit. Reuters 11.07.2007]
-*[http://www.expatica.com/actual/article.asp?subchannel_id=52&story_id=37167 Germany plans unmanned moon mission ]
+* [http://www.expatica.com/actual/article.asp?subchannel_id=52&story_id=37167 Germany plans unmanned moon mission ] {{Webarchive|url=https://web.archive.org/web/20070929102601/http://www.expatica.com/actual/article.asp?subchannel_id=52&story_id=37167 |date=2007-09-29 }}
-*[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]
+[[Kategori:Misi ke Bulan]]
+[[Kategori:Penjelajahan Bulan]]
+{{wahanaantariksa-stub}}
-[[Kategori:Penjelajahan bulan]]