প্রোটন-এম: সংশোধিত সংস্করণের মধ্যে পার্থক্য

বিষয়বস্তু বিয়োগ হয়েছে বিষয়বস্তু যোগ হয়েছে
"Proton-M" পাতাটি অনুবাদ করে তৈরি করা হয়েছে
১ নং লাইন:
{{Infobox rocket
|image = On the launch pad.jpg
|caption = Proton-M rocket on the launchpad at [[Baikonur Cosmodrome]]
 
|manufacturer = [[Khrunichev State Research and Production Space Center|Khrunichev]]
|function = [[Heavy-lift launch vehicle]]
|country-origin = [[রাশিয়া]]
|cpl = US$65 million<ref name=gao-surplus>{{cite report|url=https://www.gao.gov/assets/690/686613.pdf|title=Surplus Missile Motors|id=GAO-17-609|publisher=United States Government Accountability Office|date=August 2017|access-date=27 November 2018}} {{PD-notice}}</ref>
 
|mass = {{cvt|705000|kg}}<ref name="ils-lv">{{cite web|url=http://www.ilslaunch.com/launch-services/ils-proton-breeze-m-launch-vehicle|title=Commercial Launch Vehicle {{!}} ILS Proton Breeze M |publisher=[[International Launch Services]]|access-date=2016-04-07}}</ref>
|height = {{cvt|58.2|m}}
|diameter = {{cvt|7.4|m}}
|stages = 3 or 4
 
|capacities =
{{Infobox rocket/Payload
|location = [[Low Earth orbit|LEO]]{{efn|{{cvt|180|km}} circular LEO 51.5° [[Orbital inclination|inclination]] from [[Baikonur Cosmodrome|Baikonur]]}}
|kilos = {{cvt|23000|kg}}<ref name="proton-performance">{{cite web|title=Proton Launch System Mission Planner's Guide – Section 2. LV Performance |url=http://www.ilslaunch.com/sites/default/files/pdf/PMPG%20Section%202.pdf|publisher=[[International Launch Services]]|date=July 2009|archive-url=https://web.archive.org/web/20130805005805/http://www.ilslaunch.com/sites/default/files/pdf/PMPG%20Section%202.pdf|access-date=June 11, 2017|archive-date=5 August 2013}}</ref>
}}
{{Infobox rocket/Payload
|location = [[Geostationary transfer orbit|GTO]] (1800 m/s)
|kilos = {{cvt|6920|kg}}<ref name=proton-performance/>
}}
{{Infobox rocket/Payload
|location = [[Geostationary transfer orbit|GTO]] (1500 m/s)
|kilos = {{cvt|6300|kg}}<ref>{{cite web|date=June 9, 2016|publisher=Spaceflightnow.com|url=http://spaceflightnow.com/2016/06/09/upgraded-proton-booster-adds-satellite-to-intelsats-fleet/ |last=Clark|first=Stephen|title=Upgraded Proton booster adds satellite to Intelsat's fleet}}</ref>
}}
{{Infobox rocket/Payload
|location = [[Geostationary orbit|GSO]]
|kilos = {{cvt|3250|kg}}<ref name=proton-performance />
}}
 
|family = [[Universal Rocket]]
| comparable = {{flatlist|
* [[Ariane 5]]
* [[Atlas V|Atlas V 551]]
* [[Delta IV Heavy]]
* [[Falcon 9 FT]]
* [[H-IIB]]
* [[Long March 5]]
}}
|status = Active
|sites = {{plainlist|
* [[Baikonur Cosmodrome|Baikonur]], [[Baikonur Cosmodrome Site 81|Site 81/24]]
* [[Baikonur Cosmodrome|Baikonur]], [[Baikonur Cosmodrome Site 200|Site 200/39]]
}}
 
|launches = 112 <!-- The counts of total launches (112), failed launches (9), partial failures (2) and successful launches (101) are up to date as of 21 July 2021 and correspond exactly to the Wikipedia article: List of Proton launches, as that article was on 21 July 2021. DO NOT CHANGE COUNTS HERE UNLESS YOU ALSO MAKE CHANGES TO THE ARTICLE: LIST OF PROTON LAUNCHES-->
|fail = 9 <!-- 5 FTO (2 x GLONASS, JCSAT-11, Ekspress-AM4R, MexSat-1), plus Arabsat-4A, Ekspress-AM4 and Ekspress-MD2/Telkom in unusable/unrecoverable orbits; AMC-14 unusable but salvaged by new owner on a different mission, still counts as a failed launch -->
|partial = 2 <!-- Yamal 402 and Ekspress-AM6 managed to reach its intended orbit under its own power -->
|success = 101
|first = 7 April 2001<ref>{{cite web|url=http://planet4589.org/space/lvdb/launch/Proton|title=Proton|work=Orbital and Suborbital Launch Database|first=Jonathan|last=McDowell|publisher=Jonathan's Space Page}}</ref>
|last = 13 December 2021
|payloads = [[GLONASS]], [[ExoMars]], [[Nauka (ISS module)]]<!-- Notable payloads -->
 
<!--Stages/boosters (optional)-->
|stagedata =
{{Infobox Rocket/Stage
|type = stage
|stageno = First
|engines = 6 [[RD-253|RD-275M]]
|name = 8S810K
|thrust = {{cvt|10532|kN}}
|SI = 285 seconds
|burntime = 108 seconds
|fuel = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[Unsymmetrical dimethylhydrazine|UDMH]]
|length = {{cvt|21.18|m}}<ref name="ils-1st-2nd">{{cite web|url=http://www.ilslaunch.com/launch-services/ils-proton-breeze-m-launch-vehicle/proton-1st-2nd-stage|title=1st and 2nd Stage {{!}} ILS Proton {{!}} Launch Vehicle|publisher=[[International Launch Services]]|access-date=2016-04-07}}</ref>
|diameter = {{cvt|7.4|m}}
|propmass = {{cvt|428300|kg}}
|empty = {{cvt|30600|kg}}
}}
 
{{Infobox Rocket/Stage
|type = stage
|stageno = Second
|engines = 3 [[RD-0210]] 1 [[RD-0211]]
|name = 8S811K
|thrust = {{cvt|2399|kN}}
|SI = 327 seconds
|burntime = 206 seconds
|fuel = N<sub>2</sub>O<sub>4</sub> / UDMH
|length = {{cvt|17.05|m}}<ref name="ils-1st-2nd"/>
|diameter = {{cvt|4.1|m}}
|propmass = {{cvt|157300|kg}}
|empty = {{cvt|11000|kg}}
}}
 
{{Infobox Rocket/Stage
|type = stage
|stageno = Third
|engines = 1 [[RD-0212]]
|name = 8S812
|thrust = {{cvt|613.8|kN}}
|SI = 325 seconds
|burntime = 238 seconds
|fuel = N<sub>2</sub>O<sub>4</sub> / UDMH
|length = {{cvt|4.11|m}}<ref name="ils-3rd">{{cite web|url=http://www.ilslaunch.com/launch-services/ils-proton-breeze-m-launch-vehicle/3rd-stage|title=3rd Stage {{!}} ILS Proton {{!}} Launch Vehicle |publisher=[[International Launch Services]]|access-date=2016-04-07}}</ref>
|diameter = {{cvt|4.1|m}}
|propmass = {{cvt|46562|kg}}
|empty = {{cvt|3500|kg}}
}}
 
{{Infobox Rocket/Stage
|type = stage
|stageno = Fourth
|diff = optional
|name = [[Briz (rocket stage)|Briz-M]]
|engines = 1 [[S5.98M]]
|thrust = {{cvt|19.62|kN}}<ref name="ils-brizm">{{cite web|url=http://www.ilslaunch.com/launch-services/ils-proton-breeze-m-launch-vehicle/breeze-m|title=Breeze M {{!}} ILS Proton {{!}} Launch Vehicle |publisher=[[International Launch Services]]|access-date=2016-04-07}}</ref>
|SI = 326 seconds
|burntime = 3000 seconds
|fuel = N<sub>2</sub>O<sub>4</sub> / UDMH
|length = {{cvt|2.61|m}}
|diameter = {{cvt|4.0|m}}
|propmass = {{cvt|19800|kg}}
|empty = {{cvt|2370|kg}}
}}
 
{{Infobox Rocket/Stage
|type = stage
|stageno = Fourth
|diff = optional
|name = [[Blok D|Blok DM-2]]
|engines = 1 [[RD-58M]]
|thrust = {{cvt|85|kN}}
|SI = 352 seconds
|burntime =
|fuel = [[RP-1]] / [[liquid oxygen|LOX]]
}}
 
{{Infobox Rocket/Stage
|type = stage
|stageno = Fourth
|diff = optional
|name = [[Blok DM-03]]
|engines = 1 [[RD-58|RD-58M/RD-58MF]]
|thrust =
|SI =
|burntime =
|fuel = RP-1 / LOX
}}
 
}}
 
'''প্রোটন-এম''', (Протон-М) [[GRAU সূচক|জিআরএইউ সূচক]] '''৮কে৮২এম''' বা '''{{বানান ভুল নয়|৮কে৮২এম}}''', [[সোভিয়েত ইউনিয়ন|সোভিয়েত]] দ্বারা উন্নয়নাধীন [[প্রোটন (রকেট পরিবার)|প্রোটন]] রকেট থেকে প্রাপ্ত একটি [[খরচযোগ্য উৎক্ষেপণ ব্যবস্থা|ব্যয়যোগ্য]] রুশ [[ভারী-উত্তোলন উৎক্ষেপণ যান]]। এটি [[খ্রুনিচেভ স্টেট রিসার্চ অ্যান্ড প্রোডাকশন স্পেস সেন্টার|ক্রুনিচেভ]] দ্বারা নির্মিত, এবং [[কাজাখস্তান|কাজাখস্তানের]] [[বাইকনুর কসমাদ্রোম|বাইকোনুর কসমোড্রোমের]] উৎক্ষেপণ মঞ্চ ৮১ ও ২০০ থেকে উৎক্ষেপিত হয়েছে। বাণিজ্যিক উৎক্ষেপণগুলি [[আন্তর্জাতিক লঞ্চ পরিষেবা|আন্তর্জাতিক উৎক্ষেপণ পরিষেবা]] (আইএলএস) দ্বারা বাজারজাত করা হয় এবং সাধারণত সাইট ২০০/৩৯ ব্যবহার করে। প্রথম প্রোটন-এম ২০০১ সালের ৭ই এপ্রিল উৎক্ষেপণ করা হয়েছিল।<ref>{{ওয়েব উদ্ধৃতি|প্রকাশক=[[International Launch Services]]|শিরোনাম=Commercial Launch Heritage {{!}} Proton Rocket|ইউআরএল=http://www.ilslaunch.com/launch-services/ils-proton-breeze-m-launch-vehicle/proton-heritage|সংগ্রহের-তারিখ=2016-04-10}}</ref>