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Daşıyıcı raket (ing. carrier rocket) - Yer səthindən kosmosa, adətən, Yerin orbitinə və ondan uzağa yük daşıması üçün istifadə olunan raket.
Yükünə görə
NASA daşıyıcı raketləri Dünya orbitindən daşıdığı yük qabiliyyətinə görə aşağıdakı kimi təsnifatlandırmışdır:
- : < 2,000 kiloqram (4,400 funt) - misal üçün
- : 2,000 to 20,000 kiloqram (4,400 to 44,100 funt) - misal üçün
- : > 20,000 to 50,000 kiloqram (44,000 to 110,000 funt) - misal üçün
- : > 50,000 kiloqram (110,000 funt) - misal üçün Saturn V
İstinadlar
- NASA Space Technology Roadmaps - Launch Propulsion Systems, p.11 2016-03-24 at the Wayback Machine: "Small: 0-2t payloads, Medium: 2-20t payloads, Heavy: 20-50t payloads, Super Heavy: >50t payloads"
- "Launch services—milestones". Arianespace. 24 November 2015 tarixində . İstifadə tarixi: 19 August 2014.
- (PDF). arianespace.com. Arianespace. 23 September 2015 tarixində orijinalından (PDF) arxivləşdirilib. İstifadə tarixi: 19 August 2014.
- HSF Final Report: Seeking a Human Spaceflight Program Worthy of a Great Nation 2019-02-16 at the Wayback Machine, October 2009, Review of U.S. Human Spaceflight Plans Committee, p. 64-66: "5.2.1 The Need for Heavy Lift ... require a “super heavy-lift” launch vehicle ... range of 25 to 40 mt, setting a notional lower limit on the size of the super heavy-lift launch vehicle if refueling is available ... this strongly favors a minimum heavy-lift capacity of roughly 50 mt ..."
Xarici keçidlər
- S. A. Kamal, A. Mirza: , 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, pp 27–33 Free Full Text
- S. A. Kamal: , Proc. 10th National Aeronautical Conf., Edited by Sheikh SR, Khan AM, Pakistan Air Force Academy, Risalpur, KP, Pakistan, 2006, pp 255–263 Free Full Text
- S. A. Kamal: , Proc. 12th IEEE INMIC, Edited by Anis MK, Khan MK, Zaidi SJH, Bahria Univ., Karachi, Pakistan, 2008, pp 294–300 (invited paper) Free Full Text
- S. A. Kamal: , 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, pp 167–177 Free Full Text
- S. A. Kamal: [sic], 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, pp 178–184 Free Full Text
- S. A. Kamal: , Space Science and the Challenges of the twenty-First Century, ISPA-SUPARCO Collaborative Seminar, Univ. of Karachi, 2005 (invited paper)
- Time lapse captured from a satellite of a rocket carrying 35 satellites
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Dasiyici raket ing carrier rocket Yer sethinden kosmosa adeten Yerin orbitine ve ondan uzaga yuk dasimasi ucun istifade olunan raket Rusiyanin kosmik dasiyicisi Qazaxistandan ucusa baslayir Yukune goreNASA dasiyici raketleri Dunya orbitinden dasidigi yuk qabiliyyetine gore asagidaki kimi tesnifatlandirmisdir lt 2 000 kiloqram 4 400 funt misal ucun 2 000 to 20 000 kiloqram 4 400 to 44 100 funt misal ucun gt 20 000 to 50 000 kiloqram 44 000 to 110 000 funt misal ucun gt 50 000 kiloqram 110 000 funt misal ucun Saturn VIstinadlarNASA Space Technology Roadmaps Launch Propulsion Systems p 11 2016 03 24 at the Wayback Machine Small 0 2t payloads Medium 2 20t payloads Heavy 20 50t payloads Super Heavy gt 50t payloads Launch services milestones Arianespace 24 November 2015 tarixinde Istifade tarixi 19 August 2014 PDF arianespace com Arianespace 23 September 2015 tarixinde orijinalindan PDF arxivlesdirilib Istifade tarixi 19 August 2014 HSF Final Report Seeking a Human Spaceflight Program Worthy of a Great Nation 2019 02 16 at the Wayback Machine October 2009 Review of U S Human Spaceflight Plans Committee p 64 66 5 2 1 The Need for Heavy Lift require a super heavy lift launch vehicle range of 25 to 40 mt setting a notional lower limit on the size of the super heavy lift launch vehicle if refueling is available this strongly favors a minimum heavy lift capacity of roughly 50 mt Xarici kecidlerS A Kamal A Mirza 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 pp 27 33 Free Full Text S A Kamal Proc 10th National Aeronautical Conf Edited by Sheikh SR Khan AM Pakistan Air Force Academy Risalpur KP Pakistan 2006 pp 255 263 Free Full Text S A Kamal Proc 12th IEEE INMIC Edited by Anis MK Khan MK Zaidi SJH Bahria Univ Karachi Pakistan 2008 pp 294 300 invited paper Free Full Text S A Kamal 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 pp 167 177 Free Full Text S A Kamal sic 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 pp 178 184 Free Full Text S A Kamal Space Science and the Challenges of the twenty First Century ISPA SUPARCO Collaborative Seminar Univ of Karachi 2005 invited paper Time lapse captured from a satellite of a rocket carrying 35 satellites