Daşıyıcı raket

Daşıyıcı raket () - 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:NASA Space Technology Roadmaps - Launch Propulsion Systems, p.11 : "Small: 0-2t payloads, Medium: 2-20t payloads, Heavy: 20-50t payloads, Super Heavy: >50t payloads"

Kiçik daşıyıcı raket: <  - misal üçün Vega
Orta daşıyıcı raket:  - misal üçün Soyuz ST
Ağır daşıyıcı raket: >  - misal üçün Ariane 5
Çox ağır daşıyıcı raket: >  - misal üçün Saturn V HSF Final Report:  Seeking a Human Spaceflight Program Worthy of a Great Nation , 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 ..."

 İstinadlar 

 Xarici keçidlər 
 S. A. Kamal, A. Mirza: 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, pp 27–33 Free Full Text
 S. A. Kamal: 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, pp 255–263 Free Full Text
 S. A. Kamal: 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, pp 294–300 (invited paper) Free Full Text
 S. A. Kamal: 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, pp 167–177 Free Full Text
 S. A. Kamal: Dot-Product Steering: A New Control Law for Satellites and Spacecrafts [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: Ellipse-Orientation Steering: A Control Law for Spacecrafts [sic] and Satellite-Launch Vehicles, 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

Kateqoriya:Kosmik uçuş
Kateqoriya:Kosmik daşıyıcı raketlər