Ракета-носач — разлика између измена
Садржај обрисан Садржај додат
м Поправљене везе: сателит → Вештачки сателит |
Спашавам 7 извора и означавам 0 мртвим. #IABot (v2.0beta9) |
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Ред 22:
[[Аријанаспејс]], европски произвођач ракета-носача, такође класификује своју [[Аријана 5|Аријану 5]] у тешку категорију, пошто је њена носивост у НЗО мало преко 20.000 килограма;<ref name=arianspace201408>
{{cite web |title=Launch services—milestones |url=http://www.arianespace.com/launch-services-ariane5/milestones.asp |publisher=Arianespace |accessdate=2014-08-19 }}</ref> поред тога, ракету [[Сојуз-2 (ракета-носач)|Сојуз-2]], коју такође користи, класификује као ракету-носач средње носивости.<ref name=arianespace2009>{{cite web |title=Welcome to French Guiana |url=http://www.arianespace.com/spaceport-intro/spaceport-brochure-2009-en.pdf |website=arianespace.com |publisher=Arianespace |accessdate=2014-08-19 |archive-url=https://web.archive.org/web/20150923185100/http://www.arianespace.com/spaceport-intro/spaceport-brochure-2009-en.pdf |archive-date=23. 09. 2015 |dead-url=yes |df= }}</ref>
== Занимљивости ==
Линија 46 ⟶ 45:
== Спољашње везе ==
{{Commonscat|Space launch vehicles by country}}
* S. A. Kamal, A. Mirza: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C66: The Multi-Stage-Q System and the Inverse-Q System for Possible application in SLV]'', Proc. IBCAST 2005, Volume 3, Control and Simulation, Edited by Hussain SI, Munir A, Kiyani J, Samar R, Khan MA, National Center for Physics, Bhurban, KP, Pakistan, (2006). стр. 27–33 [http://www.ngds-ku.org/Papers/C66.pdf Free Full Text]
* S. A. Kamal: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C67: Incorporating Cross-Range Error in the Lambert Scheme]'', Proc. 10th National Aeronautical Conf., Edited by Sheikh SR, Khan AM, Pakistan Air Force Academy, Risalpur, KP, Pakistan, (2006). стр. 255–263 [http://www.ngds-ku.org/Papers/C67.pdf Free Full Text]
* S. A. Kamal: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C72: The Multi-Stage-Lambert Scheme for Steering a Satellite-Launch Vehicle]'', Proc. 12th IEEE INMIC, Edited by Anis MK, Khan MK, Zaidi SJH, Bahria Univ., Karachi, Pakistan, (2008). стр. 294–300 (invited paper) [http://www.ngds-ku.org/Papers/C72.pdf Free Full Text]
* S. A. Kamal: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C56: Incompleteness of Cross-Product Steering and a Mathematical Formulation of Extended-Cross-Product Steering]'', Proc. IBCAST 2002, Volume 1, Advanced Materials, Computational Fluid Dynamics and Control Engineering, Edited by Hoorani HR, Munir A, Samar R, Zahir S, National Center for Physics, Bhurban, KP, Pakistan, (2003). стр. 167–177 [http://www.ngds-ku.org/Papers/C56.pdf Free Full Text]
* S. A. Kamal: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C55: Dot-Product Steering: A New Control Law for Satellites and Spacecrafts]'', Proc. IBCAST 2002, Volume 1, Advanced Materials, Computational Fluid Dynamics and Control Engineering, Edited by Hoorani HR, Munir A, Samar R, Zahir S, National Center for Physics, Bhurban, KP, Pakistan, (2003). стр. 178–184 [http://www.ngds-ku.org/Papers/C55.pdf Free Full Text]
* S. A. Kamal: ''[https://web.archive.org/web/20100414071325/http://www10.brinkster.com/drakamal/pub/confabst.htm#C64: Ellipse-Orientation Steering: A Control Law for Spacecrafts and Satellite-Launch Vehicles]'', Space Science and the Challenges of the twenty-First Century, ISPA-SUPARCO Collaborative Seminar, Univ. of Karachi, 2005 (invited paper)
[[Категорија:Космонаутика]]
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