Pengguna:Steffanus kristanto: Perbedaan antara revisi
Konten dihapus Konten ditambahkan
Tidak ada ringkasan suntingan |
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* [[teknologi]] |
* [[teknologi]] |
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* [[NASA]] |
* [[NASA]] |
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{{Infobox rocket |
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|image =KSC-95EC-0911.jpg |
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|caption =Pesawat Ulang Alik ''[[pesawat ulang alik atlantis|Atlantis]]'' dalam proses peluncuran |
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|name = Pesawat Ulang Alik |
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|fungsi = Pesawat luar angkasa berawak |
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|manufaktur = [[United Space Alliance]]:{{br}}[[Thiokol]]/[[Boeing]] (SRBs){{br}}[[Lockheed Martin]] ([[Martin Marietta]]) - (ET){{br}}[[Boeing Integrated Defense Systems|Rockwell International]] (orbiter) |
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|negara = USA |
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|tinggi = 58.12 [[meter|m]] |
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|alt-height = 149.6 [[foot (unit)|ft]] |
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|diameter = 8.7 m |
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|alt-diameter = 28.5 ft |
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|massa = 2,029,203 [[kilogram|kg]] |
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|alt-mass = 4,474,574 [[pound (massa)|lb]] |
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|tingkat = 2 |
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|muatan ORB = 24,400 kg |
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|alt-LEO = 53,700 lb |
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|payload-location = [[Geostationary transfer orbit|GTO]] |
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|payload = 3,810 kg |
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|alt-payload = 8,390 lb |
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|status = Aktif |
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|lokasi = [[Kennedy Space Center Launch Complex 39|LC-39]], [[Kennedy Space Center]]{{br}}[[Vandenberg AFB Space Launch Complex 6|SLC-6]], [[Vandenberg Air Force Base|Vandenberg AFB]] (unused) |
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|diluncurkan = 117 |
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|berhasil = 115 |
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|muatan = [[International Space Station|International Space Station components]]{{br}}[[Hubble Space Telescope]]{{br}}[[Galileo spacecraft|Galileo]]{{br}}[[Magellan probe|Magellan]]{{br}}[[Chandra X-Ray Observatory|Chandra X-ray Observatory]] |
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|gagal = 2 |
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|pertama = [[April 12]] [[1981]] |
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|plannedretirement=[[2010]] |
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|pendorong = 2 |
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|nama pendorong=[[Space Shuttle Solid Rocket Booster|Solid Rocket Boosters]] |
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|mesin pendorong = 1 [[Solid-fuel rocket|solid]] |
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|kekuatan pendorong = 12,455 [[newton|kN]] |
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|alt-boosterthrust = approx. 3,300,000 [[pound force|lb<sub>f</sub>]] each, sea level liftoff |
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|boosterSI = 269 sec |
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|boostertime = 124 seconds |
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|boosterfuel = padatan |
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|stage1name = [[Shuttle External Tank|External Tank]] |
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|stage1engines =(none) {{br}} (3 [[Space Shuttle main engine|SSME]]s located on Orbiter) |
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|stage1thrust =5,253 kN |
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|alt-stage1thrust = 1,125,000 lb<sub>f</sub> combined total, sea level liftoff |
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|stage1SI =455 sec |
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|stage1time =480 seconds |
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|stage1fuel =[[Liquid oxygen|LOX]]/[[Liquid hydrogen|LH2]] |
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|stage2name =[[Space Shuttle Orbiter|Orbiter]] |
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|stage2engines =2 [[Orbital Maneuvering System|OME]] |
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|stage2thrust =53.378 kN |
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|alt-stage2thrust =12,000 lb<sub>f</sub> combined total vacuum thrust |
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|stage2SI = 316 sec |
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|stage2time =1250 seconds |
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|stage2fuel =[[Nitrogen|GN2]]}} |
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Revisi per 10 November 2014 05.36
Menyukai
 Pesawat Ulang Alik Atlantis dalam proses peluncuran | |
| Ukuran | |
|---|---|
| Diameter | 8.7 m (28.5 ft) |
| Kapasitas | |
| Muatan ke GTO |
3,810 kg (8,390 lb) |
| Sejarah peluncuran | |
| Status | Aktif |
| First stage - External Tank | |
| Mesin | (none) (3 SSMEs located on Orbiter) |
| Gaya dorong | 5,253 kN (1,125,000 lbf combined total, sea level liftoff) |
| Impuls spesifik | 455 sec |
| Durasi pembakaran | 480 seconds |
| Bahan bakar | LOX/LH2 |
| Tahapan kedua - Orbiter | |
| Mesin | 2 OME |
| Gaya dorong | 53.378 kN (12,000 lbf combined total vacuum thrust) |
| Impuls spesifik | 316 sec |
| Durasi pembakaran | 1250 seconds |
| Bahan bakar | GN2 |