Изворни код странице Poređenje orbitalnih sistema za lansiranje na čvrsto gorivo

Ovaj članak sadrži sisteme za lansiranje tereta napravljene od nekih faza na [[Rakete na čvrsto gorivo|čvrsto gorivo]] '''osim završne faze'''.

== Sve faze na čvrsto gorivo ==

{|class="wikitable sortable" style="font-size:96%;"
! width="100px" |Vozilo
! Broj faza
! width="150px" align="center"|Poreklo
! Proizvođač
! Visina (m)
! Prečnik (m)
! Težina (t)
! align="center"|Masa u<br />[[Low Earth orbit|LEO]]<br />(kg)
! Masa u<br />Drugu orbitu<br />(kg)
! Prvo poletanje
! Penzionisan
! Zapis
! Status
|-
| [[ASLV]]
| 5
| {{Flag|Indija}}
| [[Indian Space Research Organisation|ISRO]]
| align="right"|24
| align="right"|1
| align="right"|41
| align="right"|150
| 
| 1987
| 1994
| align="center"|2/4
| {{no|Penzionisan}}
|-
| [[Epsilon (rocket)|Epsilon]]<br />(without PBS)
| 3
| {{Flag|Japan}}
| [[IHI Corporation|IHI]] AeroSpace
| align="right"|24.4
| align="right"|2.6
| align="right"|90.8
| 
| 
| 2016
| -
| align="center"|1/1<!-- First Epsiron (flown in 2013) was PBS version. See [[#Partial liquid fueled]].-->
| {{yes|Aktivan}}
|-
| [[J-I]]
| 2(+1)
| {{Flag|Japan}}
| [[Japan Aerospace Exploration Agency|NASDA]] / [[Institute of Space and Astronautical Science|ISAS]]
| align="right"|33.1
| align="right"|1.8
| align="right"|88.5
| align="right"|1000
| 
| 1996
| 1996
| align="center"|1/1*
| {{no|Penzionisan}}
|-
| [[Kaituozhe-1]]
| 4
| {{Flag|Kina}}
| [[China Aerospace Science and Industry Corporation|CASIC]]
| align="right"|13.6
| align="right"|1.4 
| 
| 
| [[Sun-synchronous orbit|SSO]]: 50
| 2002
| ?
| align="center"|0/2
| align="center"|{{?}}
|-
| [[Kaituozhe (rocket family)#Kaituozhe-2 2|Kaituozhe-2]]	 
| 
| {{Flag|Kina}}
| [[China Aerospace Science and Industry Corporation|CASIC]]
| 
| 
|
| 
| 
| 2017
|
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Kuaizhou-11]]
| 4
| {{Flag|Kina}}
| [[China Aerospace Science and Industry Corporation|CASIC]]
| ?
| 2.2
| 78
| 1500
| SSO: 1000@700&nbsp;km
| 2017
| -
| -
| {{partial|U razvoju}}
|-
| [[Lambda (rocket)|L-4S]]
| 4
| {{Flag|Japan}}
| [[University of Tokyo|Tokyo univ.]]
| align="right"|16.5
| align="right"|0.735
| align="right"|9.4
| align="right"|26
| 
| 1966
| 1970<ref>{{Cite web|url=http://www.isas.jaxa.jp/en/missions/spacecraft/past/ohsumi.html|title=OHSUMI &#124; Spacecraft}}</ref>
| align="center"|1/5
| {{no|Penzionisan}}
|-
| [[Minotaur I]]
| 4
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|19.2
| align="right"|1.67
| align="right"|36.2
| align="right"|580
| SSO: 331
| 2000
| -
| align="center"|11/11
| {{yes|Aktivan}}
|-
| [[Minotaur IV]] Lite
| 3
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|23.88
| align="right"|2.34
| align="right"|86.3
| -
| 
| 2010
| -
| align="center"|2/2*
| {{yes|Aktivan}}
|-
| [[Minotaur IV]]
| 4
| {{Flag|SAD}}
| Orbital Sciences
| align="right"|23.88<ref>{{Cite web|url=https://spaceflightnow.com/minotaur/stps26/101118preview/|title=Spaceflight Now &#124; Minotaur Launch Report &#124; Minotaur rocket poised to send research to new heights}}</ref>
| align="right"|2.34
| align="right"|86.3
| align="right"|1735
| 
| 2010
| -
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Minotaur IV|Minotaur IV+]]
| 4
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|23.88
| align="right"|2.34
| align="right"|86.3
| align="right"|1985
| 
| 2011
|
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Minotaur IV]]/Orion 38
| 4
| {{Flag|SAD}}
| Orbital Sciences
| 
| 
| 
| 
| 
| 2017
| -
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Minotaur V]]
| 5
| {{Flag|SAD}}
| [[Orbital Sciences]]
| 
| align="right"|1.67
| 
| 
| [[Geosynchronous transfer orbit|GTO]]:640 [[Trans Lunar Injection|TLI]]:447
| 2013 <ref>{{cite web| url = https://www.nasa.gov/smallsat-institute/sst-soa/integration-launch-and-deployment| title = 10.0 Integration, Launch, and Deployment {{!}} NASA| date = 16 October 2021}}</ref>
| -
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Mu (rocket)|M-3C]]
| 3
| {{Flag|Japan}}
| [[University of Tokyo|Tokyo univ.]]
| align="right"|20.2
| align="right"|1.41
| align="right"|41.8
| align="right"|195
| 
| 1974
| 1979
| align="center"|3/4
| {{no|Penzionisan}}
|-
| [[Mu (rocket)|M-3H]]
| 3
| {{Flag|Japan}}
| [[University of Tokyo|Tokyo univ.]]
| align="right"|23.8
| align="right"|1.41
| align="right"|48.7
| align="right"|300
| 
| 1977
| 1978
| align="center"|3/3
| {{no|Penzionisan}}
|-
| [[Mu (rocket)|M-3S]]
| 3
| {{Flag|Japan}}
| [[University of Tokyo|Tokyo univ.]]
| align="right"|23.8
| align="right"|1.41
| align="right"|48.7
| align="right"|300
| 
| 1980
| 1984
| align="center"|4/4
| {{no|Penzionisan}}
|-
| [[Mu (rocket)|M-3SII]]
| 3(+1)
| {{Flag|Japan}}
| [[Institute of Space and Astronautical Science|ISAS]]
| align="right"|27.8
| align="right"|1.41
| align="right"|61
| align="right"|770
| 
| 1985
| 1995
| align="center"|7/8
| {{no|Penzionisan}}
|-
| [[Mu (rocket)|M-4S]]
| 4
| {{Flag|Japan}}
| [[University of Tokyo|Tokyo univ.]]
| align="right"|23.6
| align="right"|1.41
| align="right"|43.6
| align="right"|180
| 
| 1970
| 1972
| align="center"|3/4
| {{no|Penzionisan}}
|-
| [[M-V]]
| 3(+1)
| {{Flag|Japan}}
| [[Institute of Space and Astronautical Science|ISAS]]
| align="right"|30.8
| align="right"|2.5
| align="right"|140
| align="right"|1850
| Interplanetary: 500
| 1997
| 2006
| align="center"|6/7
| {{no|Penzionisan}}
|-
| [[Pegasus (rocket)|Pegasus]]
| 3
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|16.9
| align="right"|1.27
| align="right"|18.5
| align="right"|375
| 
| 1990
| 
| align="center"|10/11
| align="center"|{{?}}
|-
| [[Pegasus rocket|Pegasus XL]]
| 3
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|17.6
| align="right"|1.27
| align="right"|23.13
| align="right"|443
| 
| 1994
| -
| align="center"|29/32
| {{yes|Aktivan}}
|-
| [[Scout (rocket)|Scout]]
| 4<ref>{{cite web| url = https://www.nasa.gov/centers/langley/news/factsheets/Scout.html| title = NASA - Scout Launch Vehicle Program}}</ref>
| {{Flag|SAD}}
| [[NASA|NACA]]
| align="right"|23
| align="right"|1.01
| align="right"|21.5
| align="right"|
| 
| 1961
| 1994
| 
| {{no|Penzionisan}}
|-
| [[Scout (rocket)|Scout-A]]
| 4
| {{Flag|SAD}}
| [[NASA|NACA]]
| align="right"|25
| align="right"|1.01
| align="right"|17.85
| align="right"|
| 
| 1965
| 1970 <ref>{{Cite web|url=http://www.designation-systems.net/dusrm/app3/lv-1.html|title = LTV SLV-1 Scout}}</ref>
| 
| {{no|Penzionisan}}
|-
| [[Shavit 2|Shavit]]
| 3
| {{Flag|Izrael}}
| [[Israel Aerospace Industries|IAI]]
| align="right"|15.3
| align="right"|1.352
| align="right"|23.2
| align="right"|160
| 
| 1988
| 1990
| align="center"|2/2
| {{no|Penzionisan}}
|-
| [[Shavit 2|Shavit]]1 (LK-A)
| 3
| {{Flag|Izrael}}
| [[Israel Aerospace Industries|IAI]]
| align="right"|17.2
| align="right"|1.352
| align="right"|27.3
| align="right"|240
| 
| 1995
| 2004
| align="center"|2/4
| {{no|Penzionisan}}
|-
| [[Shavit 2|Shavit]]2 (LK-1)
| 3
| {{Flag|Izrael}}
| [[Israel Aerospace Industries|IAI]]
| align="right"|19.5
| align="right"|1.352
| align="right"|31.2
| align="right"|350
| 
| 2007
| -
| align="center"|4/4
| {{yes|Aktivan}}
|-
| [[Satellite Launch Vehicle|SLV]]
| 4
| {{Flag|Indija}}
| [[Indian Space Research Organisation|ISRO]]
| align="right"|22
| align="right"|1
| align="right"|17
| align="right"|40
| 
| 1979
| 1983
| align="center"|3/4
| {{no|Penzionisan}}
|-
| [[RPS-420]]
| 4
| {{Flag|Indonezija}}
| [[National Institute of Aeronautics and Space|LAPAN]]
| align="right"|9.5
| align="right"|0.42
| align="right"|
| align="right"|50
| 
| (2014)
| -
| align="center"|0/0
| {{partial|U razvoju}}
|-
| [[SPARK (rocket)|SPARK]]<br />(Super Strypi)
| 3
| {{Flag|SAD}}
| [[University of Hawaii|Hawaii]], [[Sandia National Laboratories|Sandia]],<br />[[Aerojet Rocketdyne]]
| 
| 
| 
| 
| SSO: 250
| 2015
| -
| align="center"|0/1
| {{yes|Aktivan}}
|-
| [[SS-520]](3-stage)
| 3
| {{Flag|Japan}}
| ISAS/[[JAXA]]
| align="right"|9.54
| align="right"|0.52
| align="right"|2.6
| align="right"|4
| -
| 2017
| -
| align="center"|1/2
| {{yes|Aktivan}}
|-
| [[Start-1]]
| 4
| {{Flag|Rusija}}
| [[Moscow Institute of Thermal Technology|MIT]]
| align="right"|22.7
| align="right"|1.61
| align="right"|47.2
| align="right"|532
| SSO: 167
| 1993
| -
| align="center"|6/6
| {{yes|Aktivan}}
|-
| [[National Space Organization (Taiwan)#SLV program|Taiwan SLV]]
| 4
| {{Flag|Kina}}
| [[National Space Organization (Taiwan)|NSPO]] 
| 
| 
| 
| align="right"|50
| 
| -
| -
| align="center"|0/0
| {{partial|U razvoju}}
|-
| [[Minotaur-C|Taurus]]
| 3+1
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|27
| align="right"|2.35
| align="right"|69
| align="right"|1259
| SSO: 889
| 1994
| -
| align="center"|5/6
| align="center"|{{?}}
|-
| [[Minotaur-C|Taurus XL<br />Minotaur-C]]
| 3+1
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|32
| align="right"|2.35
| align="right"|77
| align="right"|1458
| SSO: 1054
| 2004
| -
| align="center"|2/4
| {{yes|Aktivan}}
|-
| [[VLS-1]]
| 3
| {{Flag|Brazil}}
| [[Brazilian Space Agency|AEB]]
| align="right"|19.5
| align="right"|1.01
| align="right"|50.7
| align="right"|380
| 
| 1997
| -
| align="center"|0/2
| {{partial|U razvoju}}
|}
:<nowiki>* </nowiki>Uključujući suborbitalnu misiju<!--(Originally, J-I is a satellite launch system).-->

== Svi stepeni na čvrsto gorivo osim gornjeg stepena ==

{|class="wikitable sortable" style="font-size:96%;"
! rowspan=2 width="100px" | Vozilo
! colspan=2 | Glavne faze
! rowspan=2 width="120px" | Poreklo
! rowspan=2 width="100px" | Proizvođač
! rowspan=2 | Visina <br />(m)
! rowspan=2 | Prečnik <br />(m)
! rowspan=2 | Težina <br />(t)
! colspan=2 | Masa u ... (kg)
! rowspan=2 | Prvo <br />uzletanje
! rowspan=2 | Penzionisan
! rowspan=2 | Zapis
! rowspan=2 | Status
|-
! Čvrsto <br /> gorivo
! Tečno <br /> gorivo
! [[Low Earth orbit|LEO]]
! Druga orbita
|-
| [[Ares I]]
| 1
| 1 
| {{Flag|SAD}}
| [[Alliant Techsystems]] / [[Boeing]]
| align="right"|94
| align="right"|5.5
| align="right"|
| align="right"|25000
| 
| (2015)
| 
| align="center"|0/0
| {{no|Otkazano}}
|-
| [[Athena I]]
| 2
| 1
| {{Flag|SAD}}
| [[Lockheed Martin]]
| align="right"|
| align="right"|
| align="right"|
| align="right"|
| 
| 1995
| 2001
| align="center"|3/4
| {{no|Penzionisan}}
|-
| [[Athena I]]c
| 2
| 1
| {{Flag|SAD}}
| [[Lockheed Martin]]<br />[[Alliant Techsystems]]
| align="right"|
| align="right"|
| align="right"|
| align="right"|
| 
| (2012)
| 
| align="center"|0/0
| {{partial|U razvoju}}
|-
| [[Athena II]]<ref>{{cite web|title=Athena Mission Planner’s Guide (MPG)|url=https://www.nasa.gov/sites/default/files/files/Athena_MPG_01-23-12.pdf|access-date=November 20, 2022}}</ref>
| 3
| 1
| {{Flag|SAD}}
| [[Lockheed Martin]]
| align="right"|30.5
| align="right"|2.36
| align="right"|120.2
| align="right"|1896
| 
| 1998
| 1999
| align="center"|2/3
| {{no|Penzionisan}}
|-
| [[Athena II]]c
| 3
| 1
| {{Flag|SAD}}
| [[Lockheed Martin]]<br />[[Alliant Techsystems]]
| align="right"|
| align="right"|
| align="right"|
| align="right"|
| 
| (2012)
| 
| align="center"|0/0
| {{partial|U razvoju}}
|-
| [[Epsilon (rocket)|Epsilon]] PBS
| 3
| 1
| {{Flag|Japan}}
| [[IHI Corporation|IHI]] AeroSpace
| align="right"|24.4
| align="right"|2.6
| align="right"|90.8
| 
| 
| 2013
| -
| align="center"|3/3
| {{yes|Aktivan}}
|-
| [[i-Space (Chinese company)#Hyperbola-1|Hyperbola-1]]
| 3
| 1
| {{Flag|Kina}}
| [[i-Space (Chinese company)|i-Space]]
| 20
| 
| 31
| 300
| 
| 2019
| - 
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Kuaizhou|Kuaizhou-1]]
| 3
| 1
| {{Flag|Kina}}
| [[China Aerospace Science and Industry Corporation|CASIC]]
| 18
| 1.4
| 32
| ~300
| SSO: 430@500&nbsp;km
| 2013
| - 
| align="center"|1/1
| {{yes|Aktivan}}
|-
| [[Kuaizhou|Kuaizhou-1A]]
| 3
| 1
| {{Flag|Kina}}
| [[China Aerospace Science and Industry Corporation|CASIC]]
| 
| 1.4
| 30
| ~300
| SSO: 200@700&nbsp;km
| 2014
| - 
| align="center"|2/2
| {{yes|Aktivan}}
|-
| [[Long March 11]]
| 3
| 1
| {{Flag|Kina}}
| 
| 
| 
| 
| 
| 
| 2015
| -
| align="center"|7/7
| {{yes|Aktivan}}
|-
| [[Minotaur IV]] [[Hydrazine Auxiliary Propulsion System|HAPS]]
|
|
| {{Flag|SAD}}
| [[Orbital Sciences]]
| align="right"|23.88
| align="right"|2.34
| align="right"|86.3
| 
| 
| 2010
| -
| align="center"|1/1
| {{yes|Aktivan}}
<!--
|-
| [[Safir (rocket)|Safir]]
| 2S
| 1L(?)
| {{IRN}}
| [[Iranian Space Agency|ISA]]
| align="right"|22
| align="right"|1.25
| align="right"|26
| 
| 
| 2007
| -
| align="center"|4/5*
| {{yes|Aktivan}}
-->
|-
| [[Vega (launcher)|Vega]]
| 3
| 1
| {{Flag|Evropska Unija}}
| [[European Space Agency|ESA]] / [[Italian Space Agency|ISA]]
| align="right"|30
| align="right"|3
| align="right"|137
| align="right"|2000(?)
| SSO: 1500
| 2012
| -
| align="center"|18/20
| {{yes|Aktivan}}
|}

== Vidi još ==

{{Portal bar|Spaceflight}}
* [[Poređenje orbitalnih raketnih motora]]
* [[Poređenje orbitalnih sistema za lansiranje]]
* [[Poređenje familija orbitalnih lansera]]
* [[Poređenje orbitalnih letelica]]
* [[Poređenje teretnih vozila svemirske stanice]]
* [[Spisak dizajna sistema za lansiranje u svemir]]
* [[Spisak orbitalnih sistema za lansiranje]]

== Reference ==
{{Reflist}}

[[Категорија:Ракете]]
[[Категорија:Ракета носач]]
[[Категорија:Ракетна горива]]
[[Категорија:Ракетна погонска горива]]
[[Категорија:Ракетна техника]]
[[Категорија:Ракетни мотори]]
[[Категорија:Ракетни системи]]
[[Категорија:Свемирска трка]]
[[Категорија:Свемирске летелице]]
[[Категорија:Свемирске мисије]]
[[Категорија:Свемирске станице]]
[[Категорија:Свемирски програм по државама]]
[[Категорија:Листа ракета]]