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Orbital Launches by Launcher Family
[edit]Family | Country | Launches | Successes | Failures | Partial failures |
Retired | Active |
---|---|---|---|---|---|---|---|
Ariane | Europe | 202 | 191 | 9 | 2 | Ariane 1,2,3,4 | Ariane 5 |
Atlas | United States | 3 | 3 | 0 | 0 | Atlas 1,2,3 | Atlas 5 |
Thor/Delta | United States | 4 | 4 | 0 | 0 | Delta 1,3 | Delta 2, 4 |
Energia | Ukraine/ Russia | 2 | 2 | 0 | 0 | ||
Falcon | United States | 7 | 4 | 3 | 0 | Falcon 1 | Falcon 9 |
H-II | Japan | 27 | 21 | 6 | 0 | H-II | H-IIA, H-IIB |
Long March | People's Republic of China | 6 | 6 | 0 | 0 | ||
Minotaur | United States | 2 | 2 | 0 | 0 | Minotaur | |
Pegasus | United States | 40 | 35 | 3 | 2 | Pegasus | |
R-7 | Russia | 1748 | 0 | 0 | Soyuz | ||
Redstone/Saturn | United States | ALL | |||||
Safir | Iran | 1 | 1 | 0 | 0 | ||
SLV | India | 2 | 2 | 0 | 0 | PSLV | |
Space Shuttle | United States | 135 | 134 | 1 | 0 | ALL | |
Titan | United States | ALL | |||||
Universal Rocket | Russia | 3 | 2 | 1 | 0 | Proton | |
Vega | Europe | 0 | 0 | 0 | 0 | Vega |
Active Launch Vehicles
[edit]Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Cost (Mil US$) |
Cost/kg (LEO) (US$) |
Launches | Status | First flight | Last flight |
---|---|---|---|---|---|---|---|---|---|---|
Ariane 5ECA | Europe | EADS Astrium | 21,000[1] | 10,050 to GTO[2] | 20,000[3] | 31 [note 1] |
Operational | 2002 | ||
Ariane 5ES | Europe | EADS Astrium | 21,000[1] | 8,000 to GTO[4] | 20,000[5] | 2 | Operational | 2008 | ||
Atlas V 401 | United States | United Launch Alliance | 9,050[6] | 6,670 to SSO 4,950 to GTO[6] |
11[6] | Operational | 2002 | |||
Atlas V 411 | United States | United Launch Alliance | 9,050[6] | 8,495 to SSO 6,075 to GTO[6] |
3[6] | Operational | 2006 | |||
Atlas V 421 | United States | United Launch Alliance | 9,050[6] | 9,050 to SSO 7,000 to GTO[6] |
3[6] | Operational | 2007 | |||
Atlas V 431 | United States | United Launch Alliance | 9,050[6] | 9,050 to SSO 7,800 to GTO[6] |
2[6] | Operational | 2005 | |||
Atlas V 501 | United States | United Launch Alliance | 8,250[6] | 5,945 to SSO 3,970 to GTO 1,500 to GEO[6] |
3[6] | Operational | 2010 | |||
Atlas V 511 | United States | United Launch Alliance | 10,950[6] | 7,820 to SSO 5,370 to GTO 1,750 to GEO[6] |
0[6] | Operational | ||||
Atlas V 521 | United States | United Launch Alliance | 13,300[6] | 9,585 to SSO 6,485 to GTO 2,760 to GEO[6] |
2[6] | Operational | 2003 | |||
Atlas V 531 | United States | United Launch Alliance | 15,300[6] | 11,160 to SSO 7,425 to GTO 3,250 to GEO[6] |
1[6] | Operational | 2010 | |||
Atlas V 541 | United States | United Launch Alliance | 17,100[6] | 12,435 to SSO 8,240 to GTO 3,730 to GEO[6] |
0[6] | Operational | ||||
Atlas V 551 | United States | United Launch Alliance | 18,500[6] | 12,435 to SSO 8,700 to GTO 3,960 to GEO[6] |
1[6] | Operational | 2006 | |||
Delta II 7920 | United States | United Launch Alliance | 5,030[note 2][7] | 3,123 to SSO[note 2][7] | 27[7] | Operational | 1998 | |||
Delta II-H 7920H | United States | United Launch Alliance | 6,097[note 2][7] | 2[7] | Operational | 2003 | ||||
Delta II-H 7925H | United States | United Launch Alliance | 2,171 to GTO 1,508 to HCO[note 2][7] |
3[7] | Operational [citation needed][note 3] |
2003 | ||||
Delta IV-H | United States | United Launch Alliance | 22,950[8] | 12,980 to GTO [8] | 5 | Operational | 2004 | |||
Delta IV-M+(4,2) | United States | United Launch Alliance | 11,750[9] | 5,740 to GTO[9] | 8[10] | Operational | 2002 | |||
Delta IV-M+(5,2) | United States | United Launch Alliance | 10,250[9] | 4,590 to GTO[9] | 0[10] | Operational |
| |||
Delta IV-M+(5,4) | United States | United Launch Alliance | 13,500[9] | 16,470 to GTO[9] | 1[10] | Operational | 2009[11] | |||
Dnepr-1 | Ukraine | Yuzhmash | 3,700[12] | €10 million.[13] | 16 | Operational | 1999 | |||
Falcon 9 | United States | SpaceX | 10,450[14][15] | 4,680 to GTO[14] | [14] | 565,359 | 2 | Operational | 2010 | |
H-IIA 202 | Japan | Mitsubishi Heavy Industries | 10,000[16] | 3,800 to GTO[16] | 7[16] | Operational | 2001 | |||
H-IIA 204 | Japan | Mitsubishi Heavy Industries | 5,800 to GTO[16] | 1[16] | Operational | 2006 | ||||
H-IIB 304 | Japan | Mitsubishi Heavy Industries | 19,000[17] | 8,000[18] | 2[19] | Operational | 2009 | |||
Long March 3B | China | CALT | 5,100[citation needed] | 10 | Operational | 1996 | ||||
Long March 3B/E | China | CALT | 11,500[citation needed] | 5,500[citation needed] | 4 | Operational | 2007 | |||
Proton | Soviet Union Russia |
Khrunichev | 21,600[20] | 6,360 to GTO[20] | [21] | 85[21] | 4,302335 [22] | Operational | 1965 | |
PSLV | India | ISRO | 3,200[23] | 1,600 to SSO 1,050 to GTO[24] |
11 | Operational | 1993 | |||
PSLV-CA | India | ISRO | 2,800[23] | 1,100 to SSO[24] | 6 | Operational | 2007 | |||
PSLV-XL | India | ISRO | 3,800[24] | 1,750 to SSO 1300 to GTO[24] |
2 | Operational | 2008 | |||
Zenit-2M (2SLB) | Ukraine | Yuzhnoye | 13,920[25] | 1 | Operational | 2007 |
Orbital Launch Vehicles In Development
[edit]Vehicle | Origin | Manufacturer | Mass to LEO (kg) |
Mass to other orbits (kg) |
Cost (Mil US$) |
Cost/kg (LEO) (US$) |
Launches | Status | First flight | Last flight |
---|---|---|---|---|---|---|---|---|---|---|
Angara 1.2 | Russia | Khrunichev | 3,800[26] | 0 | Development | |||||
Angara A3 | Russia | Khrunichev | 14,600[26] | 2,400-3,600 to GTO[26] | €50 million[13] | 0 | Development | |||
Angara A5 | Russia | Khrunichev | 24,500 (63°) [27][28] | 0 | Development | |||||
Angara A7 | Russia | Khrunichev | 41,000[27][28] | 0 | Development | |||||
Falcon Heavy | United States | SpaceX | 53,000[29] | 19,000 to GTO[29] 16,000 to TLI[29] |
80-125 | 2,204 | 0 | Development | ||
GSLV Mk.III | India | ISRO[30] | 10,000 | 4,500 - 5,000[31] | 0 | Development | ||||
Long March 2F/G | China | CALT | 0 | Development | ||||||
Rus-M | Russia | TsSKB-Progress | 35,500-54,000 [32][33] | 7,500-11,500 to GTO[32][34] | 0 | Development [note 4] |
||||
Space Launch System | United States | Alliant Techsystems (SRBs) Lockheed Martin Stage I |
70,000 — 130000[35] | 0 | Development |
Retired Launch Vehicles
[edit]References
[edit]- ^ a b "Ariane 5 Users Manual, Issue 4, P. 39 (ISS orbit)" (PDF). Arianespace. Archived from the original (PDF) on 2007-09-27. Retrieved 2007-11-13.
- ^ "Ariane 5 delivers a record performance with two payloads for new Arianespace customers". Arianespace. Retrieved 2011-04-11.
- ^ "Rising Launch Prices Buoy Arianespace's Outlook". Space.com. Retrieved 2007-01-17.
- ^ a b c d e f g h http://space.skyrocket.de/doc_lau/ariane5.htm
- ^ "Rising Launch Prices Buoy Arianespace's Outlook". Space.com. Retrieved 2007-01-17.
- ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad Gunter, Krebs. "Atlas-5". Gunter's Space Page. Retrieved 1 August 2011.
- ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai aj ak al am an ao ap aq ar as at au av aw ax ay az ba bb bc bd be bf Cite error: The named reference
GSP-Delta
was invoked but never defined (see the help page). - ^ a b "Delta Product Sheet, FINAL" (PDF). United Launch Alliance. Archived from the original (PDF) on 2007-09-28. Retrieved 2007-11-14.
- ^ a b c d e f Space launch report -Delta4
- ^ a b c d e f Gunter, Krebs. "Delta-4". Gunter's Space Page. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ New communications craft launched for U.S. military, Spaceflight Now, 5 Dec 2009
- ^ Gunter, Krebs. "Dnepr-1". Gunter's Space Page. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ a b European Space Directory 2006. Referenced in: Brian Harvey, The Rebirth of the Russian Space Program. p.296.
- ^ a b c "FALCON 9 OVERVIEW". SpaceX.
- ^ "Falcon 9 Overview". Space Exploration Technologies. Retrieved 29 Oct 2010.
- ^ a b c d e f g h i Gunter, Krebs. "H-2A". Gunter's Space Page. Retrieved 1 August 2011.
- ^ "Development Plan for Future Mission from HTV System, P. 6 (Table 4 Cargo transfer capabilities)" (PDF). Jaxa. Retrieved 28 August 2008. [dead link]
- ^ "H-IIB Launch Vehicle, P. 2" (PDF). Jaxa. Retrieved 3 September 2008.
- ^ a b Cite error: The named reference
slr_launchstats
was invoked but never defined (see the help page). - ^ a b "Proton Launch System Mission Planner's Guide, LKEB-9812-1990" (PDF). International Launch Services. pp. 2–2. Archived from the original on 2007-10-27. Retrieved 2007-11-12.
LEO i = 51.6°, H = 200 km circular ... GTO (1800 m/s from GSO) i = 31.0°, Hp = 2100 km, Ha = 35,786 km
- ^ a b c d "Space Transportation Costs: Trends in Price Per Pound to Orbit 1990-2000" (PDF). Futron. Retrieved 2010-05-02.
- ^ Encyclopedia Astronautica - Proton
- ^ a b "PSLV variants capability". ISRO. Retrieved 15 May 2010.
- ^ a b c d Gunter, Krebs. "PSLV". Gunter's Space Page. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ a b Space launch report -zenit
- ^ a b c "Angaga Launch Vehicle Family". Khrunichev. Cite error: The named reference "khru_angara" was defined multiple times with different content (see the help page).
- ^ a b Семейство ракет-носителей «Ангара», date unknown, Retrieved 2010-08-09.
- ^ a b http://www.russianspaceweb.com/angara7.html
- ^ a b c "SpaceX Brochure" (PDF). Retrieved 14 June 2011.
- ^ Geosynchronous Satellite Launch Vehicle Mark III, ISRO
- ^ "GSLV MK3 (LVM3)". ISRO. 2009. Retrieved 26 December 2010.
- ^ a b Zak, Anatoly (2009). "Launch vehicle for the PPTS spacecraft". RussianSpaceWeb.com. Retrieved 2009-08-22.
- ^ http://ru.wikipedia.org/wiki/Русь-М#cite_note-novosti-kosmonavtiki-0
- ^ http://ru.wikipedia.org/wiki/Русь-М#cite_note-novosti-kosmonavtiki-0
- ^ Cite error: The named reference
naa
was invoked but never defined (see the help page). - ^ a b c d e f g h i j k l m n o p q r s t u v w x y z aa ab ac ad ae af ag ah ai aj ak al am an ao ap aq ar as at au av aw ax ay az Gunter, Krebs. "Ariane-1, -2, -3, -4". Gunter's Space Page. Retrieved 2 August 2011.
- ^ a b c Flight V193 was the seventh Ariane 5 launch of 2009 and used the last of the GS version of the launcher.
- ^ a b c d e f g h i j k l m n o p q r s t u v w Gunter, Krebs. "Atlas Centaur". Gunter's Space Page. Retrieved 1 August 2011.
- ^ Wade, Mark. "Delta 0900". Encyclopedia Astronautica. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ a b Wade, Mark. "Delta 2913". Encyclopedia Astronautica. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 4000". Encyclopedia Astronautica. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ Wade, Mark. "Delta 5000". Encyclopedia Astronautica. Archived from the original on 2 August 2011. Retrieved 2 August 2011.
- ^ a b c d "S.P.Korolev RSC Energia - LAUNCHERS". Energia.
- ^ Cite error: The named reference
Energia3
was invoked but never defined (see the help page). - ^ a b c Gunter, Krebs. "H-2". Gunter's Space Page. Retrieved 1 August 2011.
- ^ Cite error: The named reference
refN1-1
was invoked but never defined (see the help page). - ^ Cite error: The named reference
refN1-2
was invoked but never defined (see the help page). - ^ Cite error: The named reference
refN1-3
was invoked but never defined (see the help page). - ^ Cite error: The named reference
refN1-4
was invoked but never defined (see the help page). - ^ Bilstein, Roger E. "Appendix C: Saturn Family/Mission Data". Stages to Saturn A Technological History of the Apollo/Saturn Launch Vehicles. NASA History Office. Retrieved 7 April 2011.
- ^ a b Cite error: The named reference
Rocket and Space Technology
was invoked but never defined (see the help page). - ^ "SP-4221 The Space Shuttle Decision- Chapter 6: ECONOMICS AND THE SHUTTLE". NASA. Retrieved 2011-01-15.
- ^ Cite error: The named reference
Saturn
was invoked but never defined (see the help page). - ^ Cite error: The named reference
Saturn V Flight History
was invoked but never defined (see the help page). - ^ [http://www.nasa.gov/mission_pages/shuttle/main/index.html
- ^ a b "Fact Sheet - TITAN IVB". United States Air Force. Retrieved 2007-11-12.
- ^ Zenit launch log
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